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 data is extracted from the following two-line orbital elements,
1 52834C 22062E 24358.51437500 .00004498 00000+0 28208-3 0 3587
2 52834 53.2147 214.6348 0001503 84.8431 157.5804 15.08831683 15
| Epoch (UTC): | 23 December 2024 12:20:42 |
| Eccentricity: | 0.0001503 |
| inclination: | 53.2147° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 214.6348° |
| argument of perigee: | 84.8431° |
| revolutions per day: | 15.08831683 |
| mean anomaly at epoch: | 157.5804° |
| orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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