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 40697U 15028A 24358.19353143 .00000367 00000-0 15663-3 0 9993
2 40697 98.5681 69.7398 0000997 95.5909 264.5387 14.30813379496372
| Epoch (UTC): | 23 December 2024 04:38:41 |
| Eccentricity: | 0.0000997 |
| inclination: | 98.5681° |
| perigee height: | 788 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 69.7398° |
| argument of perigee: | 95.5909° |
| revolutions per day: | 14.30813379 |
| mean anomaly at epoch: | 264.5387° |
| orbit number at epoch: | 49637 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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