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 62650U 26145.15504733 +.00000000 +00000-0 +36606-3 0 00002
2 62650 97.3963 226.8852 0002806 67.7298 292.4239 15.28736708 04
| Epoch (UTC): | 25 May 2026 03:43:16 |
| Eccentricity: | 0.0002806 |
| inclination: | 97.3963° |
| perigee height: | 478 km |
| apogee height: | 482 km |
| right ascension of ascending node: | 226.8852° |
| argument of perigee: | 67.7298° |
| revolutions per day: | 15.28736708 |
| mean anomaly at epoch: | 292.4239° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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