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 60235U 26041.31955784 +.00000000 +00000-0 +23886-3 0 00004
2 60235 61.9948 312.3223 0062361 106.5246 254.2707 15.00450051 01
| Epoch (UTC): | 10 February 2026 07:40:09 |
| Eccentricity: | 0.0062361 |
| inclination: | 61.9948° |
| perigee height: | 522 km |
| apogee height: | 609 km |
| right ascension of ascending node: | 312.3223° |
| argument of perigee: | 106.5246° |
| revolutions per day: | 15.00450051 |
| mean anomaly at epoch: | 254.2707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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