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 62730U 26145.63147590 +.00000000 +00000-0 +20450-3 0 00008
2 62730 97.6548 314.9920 0014857 88.0611 272.2320 15.11145945 00
| Epoch (UTC): | 25 May 2026 15:09:19 |
| Eccentricity: | 0.0014857 |
| inclination: | 97.6548° |
| perigee height: | 522 km |
| apogee height: | 543 km |
| right ascension of ascending node: | 314.9920° |
| argument of perigee: | 88.0611° |
| revolutions per day: | 15.11145945 |
| mean anomaly at epoch: | 272.2320° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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