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 53852U 26145.46760144 +.00000000 +00000-0 +40126-4 0 00003
2 53852 53.2132 304.3795 0001070 93.4445 266.6670 15.08835465 07
| Epoch (UTC): | 25 May 2026 11:13:20 |
| Eccentricity: | 0.0001070 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 304.3795° |
| argument of perigee: | 93.4445° |
| revolutions per day: | 15.08835465 |
| mean anomaly at epoch: | 266.6670° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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