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 26087.43851808 +.00000000 +00000-0 +62439-4 0 00003
2 26932 67.0536 101.6502 0008695 263.0868 96.9244 14.31270336 01
| Epoch (UTC): | 28 March 2026 10:31:27 |
| Eccentricity: | 0.0008695 |
| inclination: | 67.0536° |
| perigee height: | 781 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 101.6502° |
| argument of perigee: | 263.0868° |
| revolutions per day: | 14.31270336 |
| mean anomaly at epoch: | 96.9244° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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