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 52463U 26145.50808609 +.00000000 +00000-0 +29274-4 0 00005
2 52463 53.2133 64.2697 0001079 94.7492 265.3624 15.08842030 04
| Epoch (UTC): | 25 May 2026 12:11:38 |
| Eccentricity: | 0.0001079 |
| inclination: | 53.2133° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 64.2697° |
| argument of perigee: | 94.7492° |
| revolutions per day: | 15.08842030 |
| mean anomaly at epoch: | 265.3624° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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