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 is defined by the following mean orbital elements,
1 32138U 99025CSG 24100.58944879 .00006105 00000-0 23355-2 0 9995
2 32138 98.9150 233.2262 0019034 295.7395 64.1822 14.30919678869990
| Epoch (UTC): | 09 April 2024 14:08:48 |
| Eccentricity: | 0.0019034 |
| inclination: | 98.9150° |
| perigee height: | 775 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 233.2262° |
| argument of perigee: | 295.7395° |
| revolutions per day: | 14.30919678 |
| mean anomaly at epoch: | 64.1822° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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