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 16682U 26067.63759259 +.00000000 +00000-0 +11277-3 0 00004
2 16682 74.0249 130.9713 0013257 53.4827 107.9198 14.37304335 00
| Epoch (UTC): | 08 March 2026 15:18:08 |
| Eccentricity: | 0.0013257 |
| inclination: | 74.0249° |
| perigee height: | 758 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 130.9713° |
| argument of perigee: | 53.4827° |
| revolutions per day: | 14.37304335 |
| mean anomaly at epoch: | 107.9198° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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