View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 36095U 26075.86512315 +.00000000 +00000-0 +46470-4 0 00002
2 36095 67.1460 117.4269 0006112 244.1541 115.8914 13.97041655 00
| Epoch (UTC): | 16 March 2026 20:45:46 |
| Eccentricity: | 0.0006112 |
| inclination: | 67.1460° |
| perigee height: | 900 km |
| apogee height: | 909 km |
| right ascension of ascending node: | 117.4269° |
| argument of perigee: | 244.1541° |
| revolutions per day: | 13.97041655 |
| mean anomaly at epoch: | 115.8914° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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