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 42784U 17036V 24007.80513513 .13611549 24273-5 31111-3 0 9994
2 42784 97.0806 52.5505 0008545 250.6889 109.3491 16.45962103364972
| Epoch (UTC): | 07 January 2024 19:19:23 |
| Eccentricity: | 0.0008545 |
| inclination: | 97.0806° |
| perigee height: | 144 km |
| apogee height: | 155 km |
| right ascension of ascending node: | 52.5505° |
| argument of perigee: | 250.6889° |
| revolutions per day: | 16.45962103 |
| mean anomaly at epoch: | 109.3491° |
| orbit number at epoch: | 36497 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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