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 16969U 26088.20730847 +.00000000 +00000-0 +88360-4 0 00008
2 16969 98.7017 81.5641 0011181 226.6060 144.9573 14.29152076 04
| Epoch (UTC): | 29 March 2026 04:58:31 |
| Eccentricity: | 0.0011181 |
| inclination: | 98.7017° |
| perigee height: | 787 km |
| apogee height: | 803 km |
| right ascension of ascending node: | 81.5641° |
| argument of perigee: | 226.6060° |
| revolutions per day: | 14.29152076 |
| mean anomaly at epoch: | 144.9573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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