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 39770U 14029E 23090.81275164 .00029840 00000-0 24781-2 0 9997
2 39770 97.9540 216.0654 0010388 212.7048 147.3384 14.98655197480557
| Epoch (UTC): | 31 March 2023 19:30:21 |
| Eccentricity: | 0.0010388 |
| inclination: | 97.9540° |
| perigee height: | 564 km |
| apogee height: | 578 km |
| right ascension of ascending node: | 216.0654° |
| argument of perigee: | 212.7048° |
| revolutions per day: | 14.98655197 |
| mean anomaly at epoch: | 147.3384° |
| orbit number at epoch: | 48055 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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