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 32953U 08025A 23335.12295429 .00000054 00000-0 31878-3 0 9996
2 32953 82.5045 213.2657 0018960 178.1274 181.9880 12.43132790704398
| Epoch (UTC): | 01 December 2023 02:57:03 |
| Eccentricity: | 0.0018960 |
| inclination: | 82.5045° |
| perigee height: | 1478 km |
| apogee height: | 1508 km |
| right ascension of ascending node: | 213.2657° |
| argument of perigee: | 178.1274° |
| revolutions per day: | 12.43132790 |
| mean anomaly at epoch: | 181.9880° |
| orbit number at epoch: | 70439 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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