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 09444U 26039.99486959 +.00000000 +00000-0 +63547-4 0 00002
2 09444 74.0483 242.8399 0013568 318.4080 41.6041 14.39322842 07
| Epoch (UTC): | 08 February 2026 23:52:36 |
| Eccentricity: | 0.0013568 |
| inclination: | 74.0483° |
| perigee height: | 751 km |
| apogee height: | 770 km |
| right ascension of ascending node: | 242.8399° |
| argument of perigee: | 318.4080° |
| revolutions per day: | 14.39322842 |
| mean anomaly at epoch: | 41.6041° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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