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 68664U 26145.22400316 +.00000000 +00000-0 +58670-3 0 00008
2 68664 97.2853 16.7456 0001784 95.8237 264.3209 15.33452986 01
| Epoch (UTC): | 25 May 2026 05:22:33 |
| Eccentricity: | 0.0001784 |
| inclination: | 97.2853° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 16.7456° |
| argument of perigee: | 95.8237° |
| revolutions per day: | 15.33452986 |
| mean anomaly at epoch: | 264.3209° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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