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 23405U 94077B 25349.95894562 .00000221 00000-0 13764-3 0 9991
2 23405 70.9812 168.6410 0004762 282.0720 77.9869 14.15551708604383
| Epoch (UTC): | 15 December 2025 23:00:52 |
| Eccentricity: | 0.0004762 |
| inclination: | 70.9812° |
| perigee height: | 837 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 168.6410° |
| argument of perigee: | 282.0720° |
| revolutions per day: | 14.15551708 |
| mean anomaly at epoch: | 77.9869° |
| orbit number at epoch: | 60438 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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