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 53893U 26145.52239101 +.00000000 +00000-0 +55312-4 0 00002
2 53893 53.2128 339.2079 0001321 90.0032 270.1111 15.08835903 00
| Epoch (UTC): | 25 May 2026 12:32:14 |
| Eccentricity: | 0.0001321 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 339.2079° |
| argument of perigee: | 90.0032° |
| revolutions per day: | 15.08835903 |
| mean anomaly at epoch: | 270.1111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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