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 26042.25389189 +.00000000 +00000-0 +85963-4 0 00008
2 32376 97.8845 227.6751 0001501 81.3769 278.7614 14.82160758 02
| Epoch (UTC): | 11 February 2026 06:05:36 |
| Eccentricity: | 0.0001501 |
| inclination: | 97.8845° |
| perigee height: | 621 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 227.6751° |
| argument of perigee: | 81.3769° |
| revolutions per day: | 14.82160758 |
| mean anomaly at epoch: | 278.7614° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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