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 is defined by the following mean orbital elements,
1 25616U 99002A 23141.79945191 .19052824 13053-5 85320-3 0 9995
2 25616 34.8977 334.6709 0008415 289.3497 70.7170 16.43115605342050
| Epoch (UTC): | 21 May 2023 19:11:12 |
| Eccentricity: | 0.0008415 |
| inclination: | 34.8977° |
| perigee height: | 152 km |
| apogee height: | 163 km |
| right ascension of ascending node: | 334.6709° |
| argument of perigee: | 289.3497° |
| revolutions per day: | 16.43115605 |
| mean anomaly at epoch: | 70.7170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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