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 59625U 26145.59598014 +.00000000 +00000-0 +17504-3 0 00009
2 59625 97.5018 223.6968 0011022 88.3447 271.9048 15.16477458 04
| Epoch (UTC): | 25 May 2026 14:18:12 |
| Eccentricity: | 0.0011022 |
| inclination: | 97.5018° |
| perigee height: | 509 km |
| apogee height: | 524 km |
| right ascension of ascending node: | 223.6968° |
| argument of perigee: | 88.3447° |
| revolutions per day: | 15.16477458 |
| mean anomaly at epoch: | 271.9048° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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