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 26045.82048523 +.00000000 +00000-0 +27421-3 0 00003
2 00011 32.8630 188.1926 1446362 80.5663 295.4988 11.90230029 07
| Epoch (UTC): | 14 February 2026 19:41:29 |
| Eccentricity: | 0.1446362 |
| inclination: | 32.8630° |
| perigee height: | 553 km |
| apogee height: | 2897 km |
| right ascension of ascending node: | 188.1926° |
| argument of perigee: | 80.5663° |
| revolutions per day: | 11.90230029 |
| mean anomaly at epoch: | 295.4988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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