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 00029U 60002B 25340.06803151 .00001316 00000-0 20708-3 0 9998
2 00029 48.3773 222.2086 0022220 157.9142 202.2733 14.78398734513556
| Epoch (UTC): | 06 December 2025 01:37:57 |
| Eccentricity: | 0.0022220 |
| inclination: | 48.3773° |
| perigee height: | 619 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 222.2086° |
| argument of perigee: | 157.9142° |
| revolutions per day: | 14.78398734 |
| mean anomaly at epoch: | 202.2733° |
| orbit number at epoch: | 51355 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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