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 62284U 26145.47073698 +.00000000 +00000-0 +53745-3 0 00004
2 62284 43.0004 142.8178 0001869 266.0791 93.9847 15.27618237 03
| Epoch (UTC): | 25 May 2026 11:17:51 |
| Eccentricity: | 0.0001869 |
| inclination: | 43.0004° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 142.8178° |
| argument of perigee: | 266.0791° |
| revolutions per day: | 15.27618237 |
| mean anomaly at epoch: | 93.9847° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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