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 53249U 26145.54907181 +.00000000 +00000-0 +25599-4 0 00003
2 53249 53.2125 209.0919 0001468 82.8452 277.2707 15.08834840 04
| Epoch (UTC): | 25 May 2026 13:10:39 |
| Eccentricity: | 0.0001468 |
| inclination: | 53.2125° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 209.0919° |
| argument of perigee: | 82.8452° |
| revolutions per day: | 15.08834840 |
| mean anomaly at epoch: | 277.2707° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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