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 39444U 26069.90185536 +.00000000 +00000-0 +62451-3 0 00008
2 39444 97.8193 39.4610 0037452 174.6735 185.4898 15.07938217 06
| Epoch (UTC): | 10 March 2026 21:38:40 |
| Eccentricity: | 0.0037452 |
| inclination: | 97.8193° |
| perigee height: | 517 km |
| apogee height: | 568 km |
| right ascension of ascending node: | 39.4610° |
| argument of perigee: | 174.6735° |
| revolutions per day: | 15.07938217 |
| mean anomaly at epoch: | 185.4898° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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