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 53858U 26145.66668980 +.00000000 +00000-0 +40448-2 0 00001
2 53858 53.2166 283.3268 0001148 39.8672 146.5143 15.69116592 04
| Epoch (UTC): | 25 May 2026 16:00:01 |
| Eccentricity: | 0.0001148 |
| inclination: | 53.2166° |
| perigee height: | 361 km |
| apogee height: | 362 km |
| right ascension of ascending node: | 283.3268° |
| argument of perigee: | 39.8672° |
| revolutions per day: | 15.69116592 |
| mean anomaly at epoch: | 146.5143° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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