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 32378U 07060A 25165.82553699 0.00000000 00000-0 00000-0 0 05
2 32378 63.9520 169.3856 7029490 266.5714 93.4286 2.00596936 02
| Epoch (UTC): | 14 June 2025 19:48:46 |
| Eccentricity: | 0.7029490 |
| inclination: | 63.9520° |
| perigee height: | 1511 km |
| apogee height: | 38847 km |
| right ascension of ascending node: | 169.3856° |
| argument of perigee: | 266.5714° |
| revolutions per day: | 2.00596936 |
| mean anomaly at epoch: | 93.4286° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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