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 26932U 26106.16599801 +.00000000 +00000-0 +32847-4 0 00007
2 26932 67.0564 53.2737 0008412 259.5558 100.4595 14.31277371 03
| Epoch (UTC): | 16 April 2026 03:59:02 |
| Eccentricity: | 0.0008412 |
| inclination: | 67.0564° |
| perigee height: | 781 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 53.2737° |
| argument of perigee: | 259.5558° |
| revolutions per day: | 14.31277371 |
| mean anomaly at epoch: | 100.4595° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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