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 694U 63047A 24282.73694635 .00007810 00000-0 96814-3 0 9997
2 694 30.3564 198.2194 0561222 214.5418 141.7466 14.08708564 58194
| Epoch (UTC): | 08 October 2024 17:41:12 |
| Eccentricity: | 0.0561222 |
| inclination: | 30.3564° |
| perigee height: | 457 km |
| apogee height: | 1270 km |
| right ascension of ascending node: | 198.2194° |
| argument of perigee: | 214.5418° |
| revolutions per day: | 14.08708564 |
| mean anomaly at epoch: | 141.7466° |
| orbit number at epoch: | 5819 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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