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 68990U 26145.27956140 +.00000000 +00000-0 +14297-3 0 00003
2 68990 97.7335 43.1271 0003921 229.9013 130.1862 14.90888156 08
| Epoch (UTC): | 25 May 2026 06:42:34 |
| Eccentricity: | 0.0003921 |
| inclination: | 97.7335° |
| perigee height: | 592 km |
| apogee height: | 598 km |
| right ascension of ascending node: | 43.1271° |
| argument of perigee: | 229.9013° |
| revolutions per day: | 14.90888156 |
| mean anomaly at epoch: | 130.1862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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