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 62950U 26145.51781800 +.00000000 +00000-0 +63061-3 0 00002
2 62950 53.1598 235.3648 0001120 81.1171 278.9957 15.31708441 00
| Epoch (UTC): | 25 May 2026 12:25:39 |
| Eccentricity: | 0.0001120 |
| inclination: | 53.1598° |
| perigee height: | 470 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 235.3648° |
| argument of perigee: | 81.1171° |
| revolutions per day: | 15.31708441 |
| mean anomaly at epoch: | 278.9957° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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