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 60101U 26145.44025613 +.00000000 +00000-0 +17510-4 0 00002
2 60101 53.1612 40.8868 0001273 86.1737 273.9409 15.30190707 04
| Epoch (UTC): | 25 May 2026 10:33:58 |
| Eccentricity: | 0.0001273 |
| inclination: | 53.1612° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 40.8868° |
| argument of perigee: | 86.1737° |
| revolutions per day: | 15.30190707 |
| mean anomaly at epoch: | 273.9409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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