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 26127.80995986 +.00000000 +00000-0 +11471-3 0 00000
2 17974 71.0079 268.1805 0011924 119.2462 346.0691 14.17650826 05
| Epoch (UTC): | 07 May 2026 19:26:20 |
| Eccentricity: | 0.0011924 |
| inclination: | 71.0079° |
| perigee height: | 825 km |
| apogee height: | 842 km |
| right ascension of ascending node: | 268.1805° |
| argument of perigee: | 119.2462° |
| revolutions per day: | 14.17650826 |
| mean anomaly at epoch: | 346.0691° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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