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 67983U 26145.48609110 +.00000000 +00000-0 +40610-3 0 00007
2 67983 97.2839 155.5876 0001361 93.4674 266.6724 15.33452106 07
| Epoch (UTC): | 25 May 2026 11:39:58 |
| Eccentricity: | 0.0001361 |
| inclination: | 97.2839° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 155.5876° |
| argument of perigee: | 93.4674° |
| revolutions per day: | 15.33452106 |
| mean anomaly at epoch: | 266.6724° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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