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 26064.16250178 +.00000000 +00000-0 +16514-3 0 00005
2 26998 74.0660 84.4325 0002993 281.0767 79.0081 14.95005104 03
| Epoch (UTC): | 05 March 2026 03:54:00 |
| Eccentricity: | 0.0002993 |
| inclination: | 74.0660° |
| perigee height: | 580 km |
| apogee height: | 584 km |
| right ascension of ascending node: | 84.4325° |
| argument of perigee: | 281.0767° |
| revolutions per day: | 14.95005104 |
| mean anomaly at epoch: | 79.0081° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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