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 17997U 26140.61250472 +.00000000 +00000-0 +70901-3 0 00006
2 17997 63.2928 275.7333 0683603 107.5562 260.1340 14.12098714 00
| Epoch (UTC): | 20 May 2026 14:42:00 |
| Eccentricity: | 0.0683603 |
| inclination: | 63.2928° |
| perigee height: | 358 km |
| apogee height: | 1346 km |
| right ascension of ascending node: | 275.7333° |
| argument of perigee: | 107.5562° |
| revolutions per day: | 14.12098714 |
| mean anomaly at epoch: | 260.1340° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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