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 62989U 26145.58335647 +.00000000 +00000-0 -11170-2 0 00009
2 62989 43.0005 258.1480 0001598 267.6526 97.9326 15.70886600 00
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001598 |
| inclination: | 43.0005° |
| perigee height: | 355 km |
| apogee height: | 357 km |
| right ascension of ascending node: | 258.1480° |
| argument of perigee: | 267.6526° |
| revolutions per day: | 15.70886600 |
| mean anomaly at epoch: | 97.9326° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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