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 00012U 59001B 23035.91055857 .00001556 00000-0 93650-3 0 9994
2 00012 32.8937 222.4655 1661093 97.6890 281.4650 11.44944802390261
| Epoch (UTC): | 04 February 2023 21:51:12 |
| Eccentricity: | 0.1661093 |
| inclination: | 32.8937° |
| perigee height: | 556 km |
| apogee height: | 3318 km |
| right ascension of ascending node: | 222.4655° |
| argument of perigee: | 97.6890° |
| revolutions per day: | 11.44944802 |
| mean anomaly at epoch: | 281.4650° |
| orbit number at epoch: | 39026 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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