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 32787U 08021E 25337.45787556 .11606960 27749-5 10987-2 0 9995
2 32787 97.6209 341.4902 0006535 227.2319 132.8430 16.38638702959840
| Epoch (UTC): | 03 December 2025 10:59:20 |
| Eccentricity: | 0.0006535 |
| inclination: | 97.6209° |
| perigee height: | 165 km |
| apogee height: | 174 km |
| right ascension of ascending node: | 341.4902° |
| argument of perigee: | 227.2319° |
| revolutions per day: | 16.38638702 |
| mean anomaly at epoch: | 132.8430° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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