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 26930U 26106.04896764 +.00000000 +00000-0 +35965-4 0 00004
2 26930 67.0025 345.8479 0010791 283.4878 76.5021 14.31574394 02
| Epoch (UTC): | 16 April 2026 01:10:30 |
| Eccentricity: | 0.0010791 |
| inclination: | 67.0025° |
| perigee height: | 779 km |
| apogee height: | 794 km |
| right ascension of ascending node: | 345.8479° |
| argument of perigee: | 283.4878° |
| revolutions per day: | 14.31574394 |
| mean anomaly at epoch: | 76.5021° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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