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 26038.00073617 +.00000000 +00000-0 +11109-3 0 00002
2 32376 97.8841 223.4845 0001547 83.2993 276.8396 14.82155295 02
| Epoch (UTC): | 07 February 2026 00:01:03 |
| Eccentricity: | 0.0001547 |
| inclination: | 97.8841° |
| perigee height: | 621 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 223.4845° |
| argument of perigee: | 83.2993° |
| revolutions per day: | 14.82155295 |
| mean anomaly at epoch: | 276.8396° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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