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 12246U 78026CP 22226.55316590 .00000156 00000-0 12974-3 0 9994
2 12246 99.2492 81.7171 0054983 253.8319 135.2993 14.02727629121025
| Epoch (UTC): | 14 August 2022 13:16:33 |
| Eccentricity: | 0.0054983 |
| inclination: | 99.2492° |
| perigee height: | 844 km |
| apogee height: | 924 km |
| right ascension of ascending node: | 81.7171° |
| argument of perigee: | 253.8319° |
| revolutions per day: | 14.02727629 |
| mean anomaly at epoch: | 135.2993° |
| orbit number at epoch: | 12102 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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