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 00029U 60002B 23266.52676087 .00001140 00000-0 19520-3 0 9995
2 00029 48.3792 75.2710 0023983 298.9192 60.9315 14.75548868394627
| Epoch (UTC): | 23 September 2023 12:38:32 |
| Eccentricity: | 0.0023983 |
| inclination: | 48.3792° |
| perigee height: | 626 km |
| apogee height: | 660 km |
| right ascension of ascending node: | 75.2710° |
| argument of perigee: | 298.9192° |
| revolutions per day: | 14.75548868 |
| mean anomaly at epoch: | 60.9315° |
| orbit number at epoch: | 39462 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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