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 62144U 26145.19246574 +.00000000 +00000-0 +62058-3 0 00000
2 62144 43.0014 93.5330 0001473 267.7572 92.3111 15.27593038 05
| Epoch (UTC): | 25 May 2026 04:37:09 |
| Eccentricity: | 0.0001473 |
| inclination: | 43.0014° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 93.5330° |
| argument of perigee: | 267.7572° |
| revolutions per day: | 15.27593038 |
| mean anomaly at epoch: | 92.3111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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