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 26063U 26039.17238038 +.00000000 +00000-0 +91995-4 0 00009
2 26063 100.1898 312.2424 0036312 40.5886 319.7992 14.37908985 04
| Epoch (UTC): | 08 February 2026 04:08:13 |
| Eccentricity: | 0.0036312 |
| inclination: | 100.1898° |
| perigee height: | 739 km |
| apogee height: | 791 km |
| right ascension of ascending node: | 312.2424° |
| argument of perigee: | 40.5886° |
| revolutions per day: | 14.37908985 |
| mean anomaly at epoch: | 319.7992° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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