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 66998U 26145.14229057 +.00000000 +00000-0 +30225-3 0 00004
2 66998 97.6358 221.2639 0016518 84.3274 275.9836 15.06526956 07
| Epoch (UTC): | 25 May 2026 03:24:53 |
| Eccentricity: | 0.0016518 |
| inclination: | 97.6358° |
| perigee height: | 535 km |
| apogee height: | 558 km |
| right ascension of ascending node: | 221.2639° |
| argument of perigee: | 84.3274° |
| revolutions per day: | 15.06526956 |
| mean anomaly at epoch: | 275.9836° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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