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 26047.92743984 +.00000000 +00000-0 +20621-3 0 00005
2 53807 53.2283 237.9515 0007328 153.0426 207.0960 15.36808083 07
| Epoch (UTC): | 16 February 2026 22:15:30 |
| Eccentricity: | 0.0007328 |
| inclination: | 53.2283° |
| perigee height: | 451 km |
| apogee height: | 461 km |
| right ascension of ascending node: | 237.9515° |
| argument of perigee: | 153.0426° |
| revolutions per day: | 15.36808083 |
| mean anomaly at epoch: | 207.0960° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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