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 40034U 14033AA 25118.86734054 .00006303 00000-0 69902-3 0 9997
2 40034 97.7306 278.2950 0046217 346.6911 13.3083 14.86827116584164
| Epoch (UTC): | 28 April 2025 20:48:58 |
| Eccentricity: | 0.0046217 |
| inclination: | 97.7306° |
| perigee height: | 575 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 278.2950° |
| argument of perigee: | 346.6911° |
| revolutions per day: | 14.86827116 |
| mean anomaly at epoch: | 13.3083° |
| orbit number at epoch: | 58416 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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