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 26049.81339350 +.00000000 +00000-0 +17826-3 0 00006
2 53807 53.2288 229.1167 0007036 157.6509 202.4804 15.36836929 02
| Epoch (UTC): | 18 February 2026 19:31:17 |
| Eccentricity: | 0.0007036 |
| inclination: | 53.2288° |
| perigee height: | 451 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 229.1167° |
| argument of perigee: | 157.6509° |
| revolutions per day: | 15.36836929 |
| mean anomaly at epoch: | 202.4804° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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