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 22830U 26088.18122543 +.00000000 +00000-0 +10655-3 0 00008
2 22830 98.4881 156.6809 0010038 221.3655 138.6770 14.32871337 07
| Epoch (UTC): | 29 March 2026 04:20:57 |
| Eccentricity: | 0.0010038 |
| inclination: | 98.4881° |
| perigee height: | 775 km |
| apogee height: | 789 km |
| right ascension of ascending node: | 156.6809° |
| argument of perigee: | 221.3655° |
| revolutions per day: | 14.32871337 |
| mean anomaly at epoch: | 138.6770° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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