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 30036U 99025NM 24277.85183812 .00011495 00000-0 26935-2 0 9992
2 30036 98.3014 309.8090 0199684 90.0018 82.9924 14.43172436928966
| Epoch (UTC): | 03 October 2024 20:26:38 |
| Eccentricity: | 0.0199684 |
| inclination: | 98.3014° |
| perigee height: | 606 km |
| apogee height: | 890 km |
| right ascension of ascending node: | 309.8090° |
| argument of perigee: | 90.0018° |
| revolutions per day: | 14.43172436 |
| mean anomaly at epoch: | 82.9924° |
| orbit number at epoch: | 92896 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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