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 50466U 26088.22034406 +.00000000 +00000-0 +16129-3 0 00001
2 50466 98.4945 181.0623 0003748 356.1334 3.9825 14.41274655 06
| Epoch (UTC): | 29 March 2026 05:17:17 |
| Eccentricity: | 0.0003748 |
| inclination: | 98.4945° |
| perigee height: | 752 km |
| apogee height: | 757 km |
| right ascension of ascending node: | 181.0623° |
| argument of perigee: | 356.1334° |
| revolutions per day: | 14.41274655 |
| mean anomaly at epoch: | 3.9825° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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