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 32287U 07054A 25093.52343140 0.00000000 00000-0 00000-0 0 02
2 32287 9.9116 52.0518 0006031 173.3270 186.6931 1.00340964 05
| Epoch (UTC): | 03 April 2025 12:33:44 |
| Eccentricity: | 0.0006031 |
| inclination: | 9.9116° |
| perigee height: | 35741 km |
| apogee height: | 35792 km |
| right ascension of ascending node: | 52.0518° |
| argument of perigee: | 173.3270° |
| revolutions per day: | 1.00340964 |
| mean anomaly at epoch: | 186.6931° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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