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 40025U 14033R 23157.28327059 .00004430 00000-0 42248-3 0 9990
2 40025 97.9976 103.8488 0010532 340.1642 19.9166 14.93835804486514
| Epoch (UTC): | 06 June 2023 06:47:54 |
| Eccentricity: | 0.0010532 |
| inclination: | 97.9976° |
| perigee height: | 578 km |
| apogee height: | 593 km |
| right ascension of ascending node: | 103.8488° |
| argument of perigee: | 340.1642° |
| revolutions per day: | 14.93835804 |
| mean anomaly at epoch: | 19.9166° |
| orbit number at epoch: | 48651 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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