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 28061U 26042.00599132 +.00000000 +00000-0 +26441-3 0 00003
2 28061 99.5605 73.9848 0145974 176.7886 183.4247 13.97739379 02
| Epoch (UTC): | 11 February 2026 00:08:37 |
| Eccentricity: | 0.0145974 |
| inclination: | 99.5605° |
| perigee height: | 795 km |
| apogee height: | 1008 km |
| right ascension of ascending node: | 73.9848° |
| argument of perigee: | 176.7886° |
| revolutions per day: | 13.97739379 |
| mean anomaly at epoch: | 183.4247° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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