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 26931U 26072.88890025 +.00000000 +00000-0 +87268-4 0 00006
2 26931 67.0499 130.7527 0007005 265.1240 94.9063 14.31914503 07
| Epoch (UTC): | 13 March 2026 21:20:00 |
| Eccentricity: | 0.0007005 |
| inclination: | 67.0499° |
| perigee height: | 780 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 130.7527° |
| argument of perigee: | 265.1240° |
| revolutions per day: | 14.31914503 |
| mean anomaly at epoch: | 94.9063° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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