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 32376U 26041.51127882 +.00000000 +00000-0 +84468-4 0 00005
2 32376 97.8844 226.9434 0001499 81.8108 278.3275 14.82159558 04
| Epoch (UTC): | 10 February 2026 12:16:14 |
| Eccentricity: | 0.0001499 |
| inclination: | 97.8844° |
| perigee height: | 621 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 226.9434° |
| argument of perigee: | 81.8108° |
| revolutions per day: | 14.82159558 |
| mean anomaly at epoch: | 278.3275° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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