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 26106.61233512 +.00000000 +00000-0 +10133-3 0 00009
2 29051 72.0033 67.5288 0066797 199.1237 160.7394 14.31487517 08
| Epoch (UTC): | 16 April 2026 14:41:45 |
| Eccentricity: | 0.0066797 |
| inclination: | 72.0033° |
| perigee height: | 739 km |
| apogee height: | 835 km |
| right ascension of ascending node: | 67.5288° |
| argument of perigee: | 199.1237° |
| revolutions per day: | 14.31487517 |
| mean anomaly at epoch: | 160.7394° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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