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 00005U 58002B 25340.86444991 .00000299 00000-0 38536-3 0 9997
2 00005 34.2440 187.8820 1840310 351.3169 5.9293 10.85934057422371
| Epoch (UTC): | 06 December 2025 20:44:48 |
| Eccentricity: | 0.1840310 |
| inclination: | 34.2440° |
| perigee height: | 650 km |
| apogee height: | 3821 km |
| right ascension of ascending node: | 187.8820° |
| argument of perigee: | 351.3169° |
| revolutions per day: | 10.85934057 |
| mean anomaly at epoch: | 5.9293° |
| orbit number at epoch: | 42237 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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