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 29051U 26103.60744014 +.00000000 +00000-0 +11223-3 0 00000
2 29051 72.0028 73.6816 0066974 204.3143 155.4831 14.31485781 07
| Epoch (UTC): | 13 April 2026 14:34:42 |
| Eccentricity: | 0.0066974 |
| inclination: | 72.0028° |
| perigee height: | 739 km |
| apogee height: | 835 km |
| right ascension of ascending node: | 73.6816° |
| argument of perigee: | 204.3143° |
| revolutions per day: | 14.31485781 |
| mean anomaly at epoch: | 155.4831° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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