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 60938U 26145.58335647 +.00000000 +00000-0 +17425-3 0 00000
2 60938 53.1388 93.7567 0008846 41.2398 166.5280 15.78080781 09
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0008846 |
| inclination: | 53.1388° |
| perigee height: | 330 km |
| apogee height: | 342 km |
| right ascension of ascending node: | 93.7567° |
| argument of perigee: | 41.2398° |
| revolutions per day: | 15.78080781 |
| mean anomaly at epoch: | 166.5280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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