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 52457U 26145.53201878 +.00000000 +00000-0 +43867-3 0 00009
2 52457 53.2121 84.1503 0001335 95.3414 264.7731 15.08804223 01
| Epoch (UTC): | 25 May 2026 12:46:06 |
| Eccentricity: | 0.0001335 |
| inclination: | 53.2121° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 84.1503° |
| argument of perigee: | 95.3414° |
| revolutions per day: | 15.08804223 |
| mean anomaly at epoch: | 264.7731° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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