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 59254U 26145.51320735 +.00000000 +00000-0 +33133-5 0 00000
2 59254 53.1600 181.1090 0001181 77.6101 282.5034 15.34389059 06
| Epoch (UTC): | 25 May 2026 12:19:01 |
| Eccentricity: | 0.0001181 |
| inclination: | 53.1600° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 181.1090° |
| argument of perigee: | 77.6101° |
| revolutions per day: | 15.34389059 |
| mean anomaly at epoch: | 282.5034° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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