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 16409U 26088.18629170 +.00000000 +00000-0 +30780-4 0 00003
2 16409 82.5385 326.0723 0015428 23.0446 337.1404 13.84924489 09
| Epoch (UTC): | 29 March 2026 04:28:15 |
| Eccentricity: | 0.0015428 |
| inclination: | 82.5385° |
| perigee height: | 935 km |
| apogee height: | 958 km |
| right ascension of ascending node: | 326.0723° |
| argument of perigee: | 23.0446° |
| revolutions per day: | 13.84924489 |
| mean anomaly at epoch: | 337.1404° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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