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 00011U 26049.59636742 +.00000000 +00000-0 +26312-3 0 00005
2 00011 32.8632 173.9059 1446229 102.0469 274.5402 11.90233821 06
| Epoch (UTC): | 18 February 2026 14:18:46 |
| Eccentricity: | 0.1446229 |
| inclination: | 32.8632° |
| perigee height: | 553 km |
| apogee height: | 2897 km |
| right ascension of ascending node: | 173.9059° |
| argument of perigee: | 102.0469° |
| revolutions per day: | 11.90233821 |
| mean anomaly at epoch: | 274.5402° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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