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 25394U 98043A 23088.84915865 .00000195 00000-0 10361-3 0 9993
2 25394 98.7836 35.6733 0000577 344.5713 15.5448 14.24488991284965
| Epoch (UTC): | 29 March 2023 20:22:47 |
| Eccentricity: | 0.0000577 |
| inclination: | 98.7836° |
| perigee height: | 810 km |
| apogee height: | 810 km |
| right ascension of ascending node: | 35.6733° |
| argument of perigee: | 344.5713° |
| revolutions per day: | 14.24488991 |
| mean anomaly at epoch: | 15.5448° |
| orbit number at epoch: | 28496 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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