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 32501U 26156.89192878 +.00000000 +00000-0 +11962-2 0 00007
2 32501 28.2343 290.6936 6749228 244.7841 33.4719 2.96724996 09
| Epoch (UTC): | 05 June 2026 21:24:22 |
| Eccentricity: | 0.6749228 |
| inclination: | 28.2343° |
| perigee height: | 272 km |
| apogee height: | 27885 km |
| right ascension of ascending node: | 290.6936° |
| argument of perigee: | 244.7841° |
| revolutions per day: | 2.96724996 |
| mean anomaly at epoch: | 33.4719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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