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 43689U 26088.17804209 +.00000000 +00000-0 +82705-4 0 00004
2 43689 98.6724 149.2164 0001957 73.2484 286.8908 14.21503381 04
| Epoch (UTC): | 29 March 2026 04:16:22 |
| Eccentricity: | 0.0001957 |
| inclination: | 98.6724° |
| perigee height: | 819 km |
| apogee height: | 822 km |
| right ascension of ascending node: | 149.2164° |
| argument of perigee: | 73.2484° |
| revolutions per day: | 14.21503381 |
| mean anomaly at epoch: | 286.8908° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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