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 62200U 26145.41006146 +.00000000 +00000-0 +60309-3 0 00004
2 62200 43.0039 197.5347 0001471 279.1648 80.9038 15.27620211 02
| Epoch (UTC): | 25 May 2026 09:50:29 |
| Eccentricity: | 0.0001471 |
| inclination: | 43.0039° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 197.5347° |
| argument of perigee: | 279.1648° |
| revolutions per day: | 15.27620211 |
| mean anomaly at epoch: | 80.9038° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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