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 53262U 26145.44874815 +.00000000 +00000-0 +11135-4 0 00005
2 53262 53.2124 209.5399 0001076 74.0198 286.0913 15.08837128 09
| Epoch (UTC): | 25 May 2026 10:46:11 |
| Eccentricity: | 0.0001076 |
| inclination: | 53.2124° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 209.5399° |
| argument of perigee: | 74.0198° |
| revolutions per day: | 15.08837128 |
| mean anomaly at epoch: | 286.0913° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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