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 60107U 26145.41071046 +.00000000 +00000-0 +10027-4 0 00002
2 60107 53.1607 40.7001 0001429 91.9972 268.1193 15.30194294 01
| Epoch (UTC): | 25 May 2026 09:51:25 |
| Eccentricity: | 0.0001429 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 40.7001° |
| argument of perigee: | 91.9972° |
| revolutions per day: | 15.30194294 |
| mean anomaly at epoch: | 268.1193° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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