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 26998U 26055.86460812 +.00000000 +00000-0 +10383-3 0 00008
2 26998 74.0666 101.1342 0002800 290.2991 69.7892 14.94977449 08
| Epoch (UTC): | 24 February 2026 20:45:02 |
| Eccentricity: | 0.0002800 |
| inclination: | 74.0666° |
| perigee height: | 580 km |
| apogee height: | 584 km |
| right ascension of ascending node: | 101.1342° |
| argument of perigee: | 290.2991° |
| revolutions per day: | 14.94977449 |
| mean anomaly at epoch: | 69.7892° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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