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 17974U 26072.97628447 +.00000000 +00000-0 +13665-3 0 00009
2 17974 71.0100 23.7891 0014799 206.9868 216.7321 14.17643590 00
| Epoch (UTC): | 13 March 2026 23:25:50 |
| Eccentricity: | 0.0014799 |
| inclination: | 71.0100° |
| perigee height: | 823 km |
| apogee height: | 844 km |
| right ascension of ascending node: | 23.7891° |
| argument of perigee: | 206.9868° |
| revolutions per day: | 14.17643590 |
| mean anomaly at epoch: | 216.7321° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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