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 52368U 26145.53568954 +.00000000 +00000-0 +41008-4 0 00007
2 52368 53.2142 204.1470 0001308 91.4768 268.6374 15.08837532 06
| Epoch (UTC): | 25 May 2026 12:51:23 |
| Eccentricity: | 0.0001308 |
| inclination: | 53.2142° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 204.1470° |
| argument of perigee: | 91.4768° |
| revolutions per day: | 15.08837532 |
| mean anomaly at epoch: | 268.6374° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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