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 39440U 26073.38908111 +.00000000 +00000-0 +61561-3 0 00004
2 39440 97.8810 22.0690 0058036 343.4169 16.5150 14.93018127 00
| Epoch (UTC): | 14 March 2026 09:20:16 |
| Eccentricity: | 0.0058036 |
| inclination: | 97.8810° |
| perigee height: | 548 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 22.0690° |
| argument of perigee: | 343.4169° |
| revolutions per day: | 14.93018127 |
| mean anomaly at epoch: | 16.5150° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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