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 16791U 26064.21076890 +.00000000 +00000-0 +28774-3 0 00009
2 16791 82.4619 148.0792 0013592 354.4959 5.6127 15.25633372 04
| Epoch (UTC): | 05 March 2026 05:03:30 |
| Eccentricity: | 0.0013592 |
| inclination: | 82.4619° |
| perigee height: | 480 km |
| apogee height: | 498 km |
| right ascension of ascending node: | 148.0792° |
| argument of perigee: | 354.4959° |
| revolutions per day: | 15.25633372 |
| mean anomaly at epoch: | 5.6127° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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