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 62201U 26145.43948772 +.00000000 +00000-0 +91611-3 0 00007
2 62201 43.0003 196.8969 0001247 270.2169 89.8540 15.27603456 05
| Epoch (UTC): | 25 May 2026 10:32:51 |
| Eccentricity: | 0.0001247 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 196.8969° |
| argument of perigee: | 270.2169° |
| revolutions per day: | 15.27603456 |
| mean anomaly at epoch: | 89.8540° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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