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 52262U 26145.35168459 +.00000000 +00000-0 +11907-3 0 00000
2 52262 53.2127 124.9231 0001623 57.1274 302.9874 15.08852798 05
| Epoch (UTC): | 25 May 2026 08:26:25 |
| Eccentricity: | 0.0001623 |
| inclination: | 53.2127° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 124.9231° |
| argument of perigee: | 57.1274° |
| revolutions per day: | 15.08852798 |
| mean anomaly at epoch: | 302.9874° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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