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 36799U 10035E 25143.50188978 .00010010 00000-0 52129-3 0 9998
2 36799 98.0603 56.4979 0004420 131.6762 228.4848 15.16224160808389
| Epoch (UTC): | 23 May 2025 12:02:43 |
| Eccentricity: | 0.0004420 |
| inclination: | 98.0603° |
| perigee height: | 514 km |
| apogee height: | 520 km |
| right ascension of ascending node: | 56.4979° |
| argument of perigee: | 131.6762° |
| revolutions per day: | 15.16224160 |
| mean anomaly at epoch: | 228.4848° |
| orbit number at epoch: | 80838 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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