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 53845U 26144.74770851 +.00000000 +00000-0 +61830-4 0 00006
2 53845 53.2135 312.7095 0001337 98.3411 261.7733 15.08838585 03
| Epoch (UTC): | 24 May 2026 17:56:42 |
| Eccentricity: | 0.0001337 |
| inclination: | 53.2135° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 312.7095° |
| argument of perigee: | 98.3411° |
| revolutions per day: | 15.08838585 |
| mean anomaly at epoch: | 261.7733° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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