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 16615U 26088.03836764 +.00000000 +00000-0 +11380-3 0 00009
2 16615 98.2216 104.6937 0010321 259.6659 158.1625 14.33304345 06
| Epoch (UTC): | 29 March 2026 00:55:14 |
| Eccentricity: | 0.0010321 |
| inclination: | 98.2216° |
| perigee height: | 773 km |
| apogee height: | 788 km |
| right ascension of ascending node: | 104.6937° |
| argument of perigee: | 259.6659° |
| revolutions per day: | 14.33304345 |
| mean anomaly at epoch: | 158.1625° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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