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 26072.39331272 +.00000000 +00000-0 +16426-3 0 00006
2 26998 74.0663 67.8646 0002991 270.8538 89.2304 14.95035844 02
| Epoch (UTC): | 13 March 2026 09:26:22 |
| Eccentricity: | 0.0002991 |
| inclination: | 74.0663° |
| perigee height: | 580 km |
| apogee height: | 584 km |
| right ascension of ascending node: | 67.8646° |
| argument of perigee: | 270.8538° |
| revolutions per day: | 14.95035844 |
| mean anomaly at epoch: | 89.2304° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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