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 62581U 26145.65371534 +.00000000 +00000-0 +77300-4 0 00008
2 62581 54.9781 10.1939 0017460 83.2710 277.0233 13.80626129 02
| Epoch (UTC): | 25 May 2026 15:41:21 |
| Eccentricity: | 0.0017460 |
| inclination: | 54.9781° |
| perigee height: | 949 km |
| apogee height: | 974 km |
| right ascension of ascending node: | 10.1939° |
| argument of perigee: | 83.2710° |
| revolutions per day: | 13.80626129 |
| mean anomaly at epoch: | 277.0233° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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