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 25774U 99031E 23152.57433826 -.00000125 00000-0 10577-4 0 9991
2 25774 51.5274 287.0335 0374787 39.3140 38.3947 13.46540709179487
| Epoch (UTC): | 01 June 2023 13:47:02 |
| Eccentricity: | 0.0374787 |
| inclination: | 51.5274° |
| perigee height: | 805 km |
| apogee height: | 1365 km |
| right ascension of ascending node: | 287.0335° |
| argument of perigee: | 39.3140° |
| revolutions per day: | 13.46540709 |
| mean anomaly at epoch: | 38.3947° |
| orbit number at epoch: | 17948 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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