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 51981U 26145.18884611 +.00000000 +00000-0 -11398-3 0 00008
2 51981 53.2131 55.7012 0001496 97.6481 262.4681 15.08851412 00
| Epoch (UTC): | 25 May 2026 04:31:56 |
| Eccentricity: | 0.0001496 |
| inclination: | 53.2131° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 55.7012° |
| argument of perigee: | 97.6481° |
| revolutions per day: | 15.08851412 |
| mean anomaly at epoch: | 262.4681° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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