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 29052U 26053.85669624 +.00000000 +00000-0 +14520-3 0 00008
2 29052 72.0300 256.0206 0038676 357.3059 2.7864 14.31515264 04
| Epoch (UTC): | 22 February 2026 20:33:38 |
| Eccentricity: | 0.0038676 |
| inclination: | 72.0300° |
| perigee height: | 759 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 256.0206° |
| argument of perigee: | 357.3059° |
| revolutions per day: | 14.31515264 |
| mean anomaly at epoch: | 2.7864° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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