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 59255U 26145.47124992 +.00000000 +00000-0 +16794-4 0 00006
2 59255 53.1601 184.3916 0001257 80.0539 280.0603 15.30189328 05
| Epoch (UTC): | 25 May 2026 11:18:35 |
| Eccentricity: | 0.0001257 |
| inclination: | 53.1601° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 184.3916° |
| argument of perigee: | 80.0539° |
| revolutions per day: | 15.30189328 |
| mean anomaly at epoch: | 280.0603° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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