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 26044.81349549 +.00000000 +00000-0 +27023-3 0 00001
2 00011 32.8629 192.0025 1446394 74.8391 300.7199 11.90228935 05
| Epoch (UTC): | 13 February 2026 19:31:26 |
| Eccentricity: | 0.1446394 |
| inclination: | 32.8629° |
| perigee height: | 553 km |
| apogee height: | 2897 km |
| right ascension of ascending node: | 192.0025° |
| argument of perigee: | 74.8391° |
| revolutions per day: | 11.90228935 |
| mean anomaly at epoch: | 300.7199° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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