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 32275U 26144.45276463 +.00000000 +00000-0 +00000-0 0 00006
2 32275 65.5906 316.7315 0001785 184.9058 175.0920 2.13103979 03
| Epoch (UTC): | 24 May 2026 10:51:58 |
| Eccentricity: | 0.0001785 |
| inclination: | 65.5906° |
| perigee height: | 19125 km |
| apogee height: | 19134 km |
| right ascension of ascending node: | 316.7315° |
| argument of perigee: | 184.9058° |
| revolutions per day: | 2.13103979 |
| mean anomaly at epoch: | 175.0920° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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