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 68491U 26144.86019640 +.00000000 +00000-0 +19716-3 0 00009
2 68491 97.7552 103.4092 0004535 114.1438 246.0255 14.91308255 05
| Epoch (UTC): | 24 May 2026 20:38:40 |
| Eccentricity: | 0.0004535 |
| inclination: | 97.7552° |
| perigee height: | 591 km |
| apogee height: | 597 km |
| right ascension of ascending node: | 103.4092° |
| argument of perigee: | 114.1438° |
| revolutions per day: | 14.91308255 |
| mean anomaly at epoch: | 246.0255° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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