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 29050U 26053.67874395 +.00000000 +00000-0 +35092-3 0 00006
2 29050 72.0129 200.3411 0042447 138.1629 222.2786 14.66608810 00
| Epoch (UTC): | 22 February 2026 16:17:23 |
| Eccentricity: | 0.0042447 |
| inclination: | 72.0129° |
| perigee height: | 642 km |
| apogee height: | 702 km |
| right ascension of ascending node: | 200.3411° |
| argument of perigee: | 138.1629° |
| revolutions per day: | 14.66608810 |
| mean anomaly at epoch: | 222.2786° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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