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 22490U 93009B 23273.11127956 .00000712 00000-0 14729-3 0 9993
2 22490 24.9685 202.0681 0042898 96.5629 286.9685 14.45015957617953
| Epoch (UTC): | 30 September 2023 02:40:14 |
| Eccentricity: | 0.0042898 |
| inclination: | 24.9685° |
| perigee height: | 711 km |
| apogee height: | 772 km |
| right ascension of ascending node: | 202.0681° |
| argument of perigee: | 96.5629° |
| revolutions per day: | 14.45015957 |
| mean anomaly at epoch: | 286.9685° |
| orbit number at epoch: | 61795 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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