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 26106.87733115 +.00000000 +00000-0 +18421-3 0 00008
2 29050 72.0118 85.1284 0042009 35.9435 324.4534 14.66800018 08
| Epoch (UTC): | 16 April 2026 21:03:21 |
| Eccentricity: | 0.0042009 |
| inclination: | 72.0118° |
| perigee height: | 642 km |
| apogee height: | 701 km |
| right ascension of ascending node: | 85.1284° |
| argument of perigee: | 35.9435° |
| revolutions per day: | 14.66800018 |
| mean anomaly at epoch: | 324.4534° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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