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 39446U 13066AG 23081.38459759 .00004932 00000-0 61585-3 0 9992
2 39446 97.7253 39.2844 0064495 262.6875 96.7005 14.81341694502167
| Epoch (UTC): | 22 March 2023 09:13:49 |
| Eccentricity: | 0.0064495 |
| inclination: | 97.7253° |
| perigee height: | 580 km |
| apogee height: | 670 km |
| right ascension of ascending node: | 39.2844° |
| argument of perigee: | 262.6875° |
| revolutions per day: | 14.81341694 |
| mean anomaly at epoch: | 96.7005° |
| orbit number at epoch: | 50216 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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