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 40021U 14033M 25114.01566809 .00031523 00000-0 12136-2 0 9995
2 40021 98.0986 124.3799 0011694 114.9287 245.3166 15.26250050591218
| Epoch (UTC): | 24 April 2025 00:22:33 |
| Eccentricity: | 0.0011694 |
| inclination: | 98.0986° |
| perigee height: | 479 km |
| apogee height: | 495 km |
| right ascension of ascending node: | 124.3799° |
| argument of perigee: | 114.9287° |
| revolutions per day: | 15.26250050 |
| mean anomaly at epoch: | 245.3166° |
| orbit number at epoch: | 59121 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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