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 30138U 99025ST 23337.61826312 .00003350 00000-0 17332-2 0 9996
2 30138 98.8301 27.1110 0022523 99.1303 54.0190 14.15476662869135
| Epoch (UTC): | 03 December 2023 14:50:17 |
| Eccentricity: | 0.0022523 |
| inclination: | 98.8301° |
| perigee height: | 824 km |
| apogee height: | 857 km |
| right ascension of ascending node: | 27.1110° |
| argument of perigee: | 99.1303° |
| revolutions per day: | 14.15476662 |
| mean anomaly at epoch: | 54.0190° |
| orbit number at epoch: | 86913 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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