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 data is extracted from the following two-line orbital elements,
1 26063U 00004C 25134.59103262 .00000138 00000-0 64873-4 0 9998
2 26063 100.2176 352.7628 0036617 81.6102 278.9228 14.37766665326000
| Epoch (UTC): | 14 May 2025 14:11:05 |
| Eccentricity: | 0.0036617 |
| inclination: | 100.2176° |
| perigee height: | 740 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 352.7628° |
| argument of perigee: | 81.6102° |
| revolutions per day: | 14.37766665 |
| mean anomaly at epoch: | 278.9228° |
| orbit number at epoch: | 32600 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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