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 00123U 61015H 22181.59363841 .00000173 00000-0 81602-4 0 9994
2 00123 66.6859 316.1383 0123425 250.2520 108.5236 14.37444074171187
| Epoch (UTC): | 30 June 2022 14:14:50 |
| Eccentricity: | 0.0123425 |
| inclination: | 66.6859° |
| perigee height: | 679 km |
| apogee height: | 855 km |
| right ascension of ascending node: | 316.1383° |
| argument of perigee: | 250.2520° |
| revolutions per day: | 14.37444074 |
| mean anomaly at epoch: | 108.5236° |
| orbit number at epoch: | 17118 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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