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 9903U 77024A 23147.72185167 .00000236 00000-0 12975-3 0 9993
2 9903 81.2698 138.0953 0036705 280.9958 78.7085 14.08465108370583
| Epoch (UTC): | 27 May 2023 17:19:27 |
| Eccentricity: | 0.0036705 |
| inclination: | 81.2698° |
| perigee height: | 838 km |
| apogee height: | 891 km |
| right ascension of ascending node: | 138.0953° |
| argument of perigee: | 280.9958° |
| revolutions per day: | 14.08465108 |
| mean anomaly at epoch: | 78.7085° |
| orbit number at epoch: | 37058 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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