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 40109U 26145.54307336 +.00000000 +00000-0 +15709-3 0 00001
2 40109 63.3791 77.5298 0388280 14.5516 346.6320 13.45439971 04
| Epoch (UTC): | 25 May 2026 13:02:01 |
| Eccentricity: | 0.0388280 |
| inclination: | 63.3791° |
| perigee height: | 799 km |
| apogee height: | 1379 km |
| right ascension of ascending node: | 77.5298° |
| argument of perigee: | 14.5516° |
| revolutions per day: | 13.45439971 |
| mean anomaly at epoch: | 346.6320° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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