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 62241U 26145.65613919 +.00000000 +00000-0 +16315-3 0 00005
2 62241 89.0128 24.4025 0015587 88.3899 271.9037 13.51009643 04
| Epoch (UTC): | 25 May 2026 15:44:50 |
| Eccentricity: | 0.0015587 |
| inclination: | 89.0128° |
| perigee height: | 1057 km |
| apogee height: | 1080 km |
| right ascension of ascending node: | 24.4025° |
| argument of perigee: | 88.3899° |
| revolutions per day: | 13.51009643 |
| mean anomaly at epoch: | 271.9037° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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