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 52465U 26145.50440963 +.00000000 +00000-0 +19009-4 0 00007
2 52465 53.2144 64.2835 0001247 87.6475 272.4660 15.08837108 00
| Epoch (UTC): | 25 May 2026 12:06:20 |
| Eccentricity: | 0.0001247 |
| inclination: | 53.2144° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 64.2835° |
| argument of perigee: | 87.6475° |
| revolutions per day: | 15.08837108 |
| mean anomaly at epoch: | 272.4660° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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