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 62601U 26145.43730546 +.00000000 +00000-0 +74732-3 0 00004
2 62601 42.9998 204.3438 0001065 263.3005 96.7726 15.27591321 06
| Epoch (UTC): | 25 May 2026 10:29:43 |
| Eccentricity: | 0.0001065 |
| inclination: | 42.9998° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 204.3438° |
| argument of perigee: | 263.3005° |
| revolutions per day: | 15.27591321 |
| mean anomaly at epoch: | 96.7726° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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