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 62976U 26145.56456472 +.00000000 +00000-0 +40678-4 0 00009
2 62976 50.0059 316.7510 0001095 95.2210 264.8787 13.29322289 01
| Epoch (UTC): | 25 May 2026 13:32:58 |
| Eccentricity: | 0.0001095 |
| inclination: | 50.0059° |
| perigee height: | 1148 km |
| apogee height: | 1150 km |
| right ascension of ascending node: | 316.7510° |
| argument of perigee: | 95.2210° |
| revolutions per day: | 13.29322289 |
| mean anomaly at epoch: | 264.8787° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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