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 45U 60007A 23033.14241325 .00000806 00000-0 22491-3 0 9990
2 45 66.6952 11.4811 0257716 335.4874 23.4144 14.34036971260287
| Epoch (UTC): | 02 February 2023 03:25:04 |
| Eccentricity: | 0.0257716 |
| inclination: | 66.6952° |
| perigee height: | 594 km |
| apogee height: | 963 km |
| right ascension of ascending node: | 11.4811° |
| argument of perigee: | 335.4874° |
| revolutions per day: | 14.34036971 |
| mean anomaly at epoch: | 23.4144° |
| orbit number at epoch: | 26028 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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