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 26039.48596743 +.00000000 +00000-0 +96527-4 0 00003
2 32376 97.8842 224.9479 0001522 82.0730 278.0655 14.82156833 02
| Epoch (UTC): | 08 February 2026 11:39:47 |
| Eccentricity: | 0.0001522 |
| inclination: | 97.8842° |
| perigee height: | 621 km |
| apogee height: | 624 km |
| right ascension of ascending node: | 224.9479° |
| argument of perigee: | 82.0730° |
| revolutions per day: | 14.82156833 |
| mean anomaly at epoch: | 278.0655° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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