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 26154.73134802 +.00000000 +00000-0 +72768-4 0 00005
2 26932 67.0563 287.8249 0007218 251.5150 108.5167 14.31291006 03
| Epoch (UTC): | 03 June 2026 17:33:08 |
| Eccentricity: | 0.0007218 |
| inclination: | 67.0563° |
| perigee height: | 782 km |
| apogee height: | 793 km |
| right ascension of ascending node: | 287.8249° |
| argument of perigee: | 251.5150° |
| revolutions per day: | 14.31291006 |
| mean anomaly at epoch: | 108.5167° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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