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 16012U 26088.21161352 +.00000000 +00000-0 +95982-4 0 00005
2 16012 74.0612 9.7138 0015313 195.4277 164.6413 14.37761301 06
| Epoch (UTC): | 29 March 2026 05:04:43 |
| Eccentricity: | 0.0015313 |
| inclination: | 74.0612° |
| perigee height: | 755 km |
| apogee height: | 777 km |
| right ascension of ascending node: | 9.7138° |
| argument of perigee: | 195.4277° |
| revolutions per day: | 14.37761301 |
| mean anomaly at epoch: | 164.6413° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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