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 62089U 26145.45911144 +.00000000 +00000-0 +24901-2 0 00003
2 62089 42.9993 300.6346 0002425 268.7091 91.3499 15.71002992 02
| Epoch (UTC): | 25 May 2026 11:01:07 |
| Eccentricity: | 0.0002425 |
| inclination: | 42.9993° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 300.6346° |
| argument of perigee: | 268.7091° |
| revolutions per day: | 15.71002992 |
| mean anomaly at epoch: | 91.3499° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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