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 40071U 14037C 24259.90407472 .00006260 00000-0 72821-3 0 9999
2 40071 98.3273 176.5266 0007708 176.5586 183.5682 14.85670667551025
| Epoch (UTC): | 15 September 2024 21:41:52 |
| Eccentricity: | 0.0007708 |
| inclination: | 98.3273° |
| perigee height: | 606 km |
| apogee height: | 617 km |
| right ascension of ascending node: | 176.5266° |
| argument of perigee: | 176.5586° |
| revolutions per day: | 14.85670667 |
| mean anomaly at epoch: | 183.5682° |
| orbit number at epoch: | 55102 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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