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 52367U 26145.42160944 +.00000000 +00000-0 +36451-4 0 00007
2 52367 53.2115 204.6590 0001032 71.9424 288.1680 15.08838952 03
| Epoch (UTC): | 25 May 2026 10:07:07 |
| Eccentricity: | 0.0001032 |
| inclination: | 53.2115° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 204.6590° |
| argument of perigee: | 71.9424° |
| revolutions per day: | 15.08838952 |
| mean anomaly at epoch: | 288.1680° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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