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 23404U 94077A 25348.91339612 .00000348 00000-0 20807-3 0 9991
2 23404 71.0145 276.7261 0013797 120.0321 240.2172 14.13906590602509
| Epoch (UTC): | 14 December 2025 21:55:17 |
| Eccentricity: | 0.0013797 |
| inclination: | 71.0145° |
| perigee height: | 836 km |
| apogee height: | 856 km |
| right ascension of ascending node: | 276.7261° |
| argument of perigee: | 120.0321° |
| revolutions per day: | 14.13906590 |
| mean anomaly at epoch: | 240.2172° |
| orbit number at epoch: | 60250 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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