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 14879U 26068.31069641 +.00000000 +00000-0 -57638-4 0 00008
2 14879 101.2860 1.0041 0213492 265.3344 223.4429 12.15607281 02
| Epoch (UTC): | 09 March 2026 07:27:24 |
| Eccentricity: | 0.0213492 |
| inclination: | 101.2860° |
| perigee height: | 1441 km |
| apogee height: | 1782 km |
| right ascension of ascending node: | 1.0041° |
| argument of perigee: | 265.3344° |
| revolutions per day: | 12.15607281 |
| mean anomaly at epoch: | 223.4429° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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