PATENT CLAIM ANALYSIS

Application Number: 15868812
Application Type: Utility
Filing Date: 2018-01
Publication Date: 2018-06
Patent Classification: ["244", "171100"]

Abstract:
A satellite system operates at altitudes between 100 and 350 km relying on vehicles including a self-sustaining ion engine to counteract atmospheric drag to maintain near-constant orbit dynamics. The system operates at altitudes that are substantially lower than traditional satellites, reducing size, weight and cost of the vehicles and their constituent subsystems such as optical imagers, radars, and radio links. The system can include a large number of lower cost, mass, and altitude vehicles, enabling revisit times substantially shorter than previous satellite systems. The vehicles spend their orbit at low altitude, high atmospheric density conditions that have heretofore been virtually impossible to consider for stable orbits. Short revisit times at low altitudes enable near-real time imaging at high resolution and low cost. At such altitudes, the system has no impact on space junk issues of traditional LEO orbits, and is self-cleaning in that space junk or disabled craft will de-orbit.

Claim (Index 25):
The ground station of  claim 23 , wherein the ground station receives data transmitted by the satellite in near real-time.

Metadata:
- Claim Count in Document: 80.0
- Percentile: 86.0
- Lexical Diversity: 1.64356
- Patent Class: 244.0
- Transitional Phrase Type: none
- Component Type: 0
- Foreign Priority: False
- Related Applications: ['15868794', '15439533', '11086754', '13876678', '13544155']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.8822692357482463
- 35 USC 102 Novelty (BERT): 0.5160802802286353
- Combined Prediction Score: 0.8456503401962853
- Mean Citation Score: 284.952148
- Max Citation Score: 331.07434
- Similarity Product: 230.34994428277017

Labels:
- Claim Label 101: 1
- Claim Label 102: 1
- Claim Label 103: 1
- Claim Label 112: 1
- Combined Label: 1
- Label 101 Adjusted: 1

Dataset: test