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 60108U 26145.40121140 +.00000000 +00000-0 +16142-4 0 00007
2 60108 53.1615 40.6414 0001157 83.0044 277.1088 15.30192164 05
| Epoch (UTC): | 25 May 2026 09:37:44 |
| Eccentricity: | 0.0001157 |
| inclination: | 53.1615° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 40.6414° |
| argument of perigee: | 83.0044° |
| revolutions per day: | 15.30192164 |
| mean anomaly at epoch: | 277.1088° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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