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 53255U 26145.46346604 +.00000000 +00000-0 -36171-4 0 00007
2 53255 53.2108 209.4703 0001468 84.8944 275.2215 15.08843457 01
| Epoch (UTC): | 25 May 2026 11:07:23 |
| Eccentricity: | 0.0001468 |
| inclination: | 53.2108° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 209.4703° |
| argument of perigee: | 84.8944° |
| revolutions per day: | 15.08843457 |
| mean anomaly at epoch: | 275.2215° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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