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 62901U 26145.52664979 +.00000000 +00000-0 +21662-3 0 00007
2 62901 45.0022 332.0406 0007605 342.7874 17.2745 15.15794459 00
| Epoch (UTC): | 25 May 2026 12:38:22 |
| Eccentricity: | 0.0007605 |
| inclination: | 45.0022° |
| perigee height: | 513 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 332.0406° |
| argument of perigee: | 342.7874° |
| revolutions per day: | 15.15794459 |
| mean anomaly at epoch: | 17.2745° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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