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 22829U 26106.93746035 +.00000000 +00000-0 +41556-4 0 00003
2 22829 98.6694 174.0860 0009246 203.5536 156.5225 14.31901345 05
| Epoch (UTC): | 16 April 2026 22:29:56 |
| Eccentricity: | 0.0009246 |
| inclination: | 98.6694° |
| perigee height: | 779 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 174.0860° |
| argument of perigee: | 203.5536° |
| revolutions per day: | 14.31901345 |
| mean anomaly at epoch: | 156.5225° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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