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 27939U 26073.61578894 +.00000000 +00000-0 +24778-3 0 00000
2 27939 98.3446 255.3138 0010774 203.3329 244.0936 14.73270096 01
| Epoch (UTC): | 14 March 2026 14:46:44 |
| Eccentricity: | 0.0010774 |
| inclination: | 98.3446° |
| perigee height: | 643 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 255.3138° |
| argument of perigee: | 203.3329° |
| revolutions per day: | 14.73270096 |
| mean anomaly at epoch: | 244.0936° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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