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 03597U 68110A 24260.69744473 .00001026 00000-0 28520-3 0 9997
2 03597 34.9944 33.4349 0005669 203.0490 156.9946 14.46713996941014
| Epoch (UTC): | 16 September 2024 16:44:19 |
| Eccentricity: | 0.0005669 |
| inclination: | 34.9944° |
| perigee height: | 732 km |
| apogee height: | 740 km |
| right ascension of ascending node: | 33.4349° |
| argument of perigee: | 203.0490° |
| revolutions per day: | 14.46713996 |
| mean anomaly at epoch: | 156.9946° |
| orbit number at epoch: | 94101 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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