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 53807U 26133.86956852 +.00000000 +00000-0 +92241-4 0 00002
2 53807 53.2285 195.0262 0007414 72.2458 287.9355 15.37844401 05
| Epoch (UTC): | 13 May 2026 20:52:10 |
| Eccentricity: | 0.0007414 |
| inclination: | 53.2285° |
| perigee height: | 447 km |
| apogee height: | 458 km |
| right ascension of ascending node: | 195.0262° |
| argument of perigee: | 72.2458° |
| revolutions per day: | 15.37844401 |
| mean anomaly at epoch: | 287.9355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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