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 53846U 26145.45793120 +.00000000 +00000-0 -63579-4 0 00003
2 53846 53.2152 309.3071 0000988 88.7183 271.3922 15.08831010 02
| Epoch (UTC): | 25 May 2026 10:59:25 |
| Eccentricity: | 0.0000988 |
| inclination: | 53.2152° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 309.3071° |
| argument of perigee: | 88.7183° |
| revolutions per day: | 15.08831010 |
| mean anomaly at epoch: | 271.3922° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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