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 60100U 26145.13361694 +.00000000 +00000-0 +35792-4 0 00001
2 60100 53.1607 41.8172 0001168 87.0362 273.0773 15.30198877 04
| Epoch (UTC): | 25 May 2026 03:12:24 |
| Eccentricity: | 0.0001168 |
| inclination: | 53.1607° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 41.8172° |
| argument of perigee: | 87.0362° |
| revolutions per day: | 15.30198877 |
| mean anomaly at epoch: | 273.0773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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