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 68668U 26145.38713311 +.00000000 +00000-0 +57111-3 0 00000
2 68668 97.2862 16.9833 0000972 95.1385 264.9968 15.33444249 02
| Epoch (UTC): | 25 May 2026 09:17:28 |
| Eccentricity: | 0.0000972 |
| inclination: | 97.2862° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 16.9833° |
| argument of perigee: | 95.1385° |
| revolutions per day: | 15.33444249 |
| mean anomaly at epoch: | 264.9968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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