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 14129U 26036.76544082 +.00000000 +00000-0 +00000-0 0 00003
2 14129 25.9610 241.7283 6056240 79.1046 339.8337 2.05870291 09
| Epoch (UTC): | 05 February 2026 18:22:14 |
| Eccentricity: | 0.6056240 |
| inclination: | 25.9610° |
| perigee height: | 3916 km |
| apogee height: | 35532 km |
| right ascension of ascending node: | 241.7283° |
| argument of perigee: | 79.1046° |
| revolutions per day: | 2.05870291 |
| mean anomaly at epoch: | 339.8337° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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