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 65850U 26145.27920922 +.00000000 +00000-0 +14662-2 0 00009
2 65850 53.1578 93.0143 0000990 84.1648 275.9466 15.30240300 01
| Epoch (UTC): | 25 May 2026 06:42:03 |
| Eccentricity: | 0.0000990 |
| inclination: | 53.1578° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 93.0143° |
| argument of perigee: | 84.1648° |
| revolutions per day: | 15.30240300 |
| mean anomaly at epoch: | 275.9466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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