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 26040.05813748 +.00000000 +00000-0 +15204-3 0 00009
2 53807 53.2293 274.8115 0007988 131.1152 229.0543 15.36715374 00
| Epoch (UTC): | 09 February 2026 01:23:43 |
| Eccentricity: | 0.0007988 |
| inclination: | 53.2293° |
| perigee height: | 450 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 274.8115° |
| argument of perigee: | 131.1152° |
| revolutions per day: | 15.36715374 |
| mean anomaly at epoch: | 229.0543° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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