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 26106.82433206 +.00000000 +00000-0 +10744-3 0 00003
2 29052 72.0313 147.7342 0040833 267.6077 92.0386 14.31569225 03
| Epoch (UTC): | 16 April 2026 19:47:02 |
| Eccentricity: | 0.0040833 |
| inclination: | 72.0313° |
| perigee height: | 757 km |
| apogee height: | 816 km |
| right ascension of ascending node: | 147.7342° |
| argument of perigee: | 267.6077° |
| revolutions per day: | 14.31569225 |
| mean anomaly at epoch: | 92.0386° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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