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 00046U 60007B 23087.70650028 .00001671 00000-0 35330-3 0 9993
2 00046 66.6910 184.7950 0199638 94.8540 267.5394 14.50328363286119
| Epoch (UTC): | 28 March 2023 16:57:21 |
| Eccentricity: | 0.0199638 |
| inclination: | 66.6910° |
| perigee height: | 583 km |
| apogee height: | 866 km |
| right ascension of ascending node: | 184.7950° |
| argument of perigee: | 94.8540° |
| revolutions per day: | 14.50328363 |
| mean anomaly at epoch: | 267.5394° |
| orbit number at epoch: | 28611 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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