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 6073U 72023E 25130.02495443 .08088373 12542-4 65849-4 0 9993
2 6073 51.9455 241.9030 0035390 103.6551 63.6433 16.48653575751319
| Epoch (UTC): | 10 May 2025 00:35:56 |
| Eccentricity: | 0.0035390 |
| inclination: | 51.9455° |
| perigee height: | 120 km |
| apogee height: | 166 km |
| right ascension of ascending node: | 241.9030° |
| argument of perigee: | 103.6551° |
| revolutions per day: | 16.48653575 |
| mean anomaly at epoch: | 63.6433° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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