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 62898U 26145.34293286 +.00000000 +00000-0 +87582-3 0 00004
2 62898 43.0003 252.0660 0001265 273.9769 86.0938 15.27602562 03
| Epoch (UTC): | 25 May 2026 08:13:49 |
| Eccentricity: | 0.0001265 |
| inclination: | 43.0003° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 252.0660° |
| argument of perigee: | 273.9769° |
| revolutions per day: | 15.27602562 |
| mean anomaly at epoch: | 86.0938° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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