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 26073.35009583 +.00000000 +00000-0 +19401-3 0 00002
2 27939 98.3446 255.0405 0010768 204.1580 274.9323 14.73267957 00
| Epoch (UTC): | 14 March 2026 08:24:08 |
| Eccentricity: | 0.0010768 |
| inclination: | 98.3446° |
| perigee height: | 643 km |
| apogee height: | 658 km |
| right ascension of ascending node: | 255.0405° |
| argument of perigee: | 204.1580° |
| revolutions per day: | 14.73267957 |
| mean anomaly at epoch: | 274.9323° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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