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 67982U 26145.49152675 +.00000000 +00000-0 +78584-3 0 00007
2 67982 97.2851 155.5783 0000769 80.0075 280.1255 15.33451362 08
| Epoch (UTC): | 25 May 2026 11:47:47 |
| Eccentricity: | 0.0000769 |
| inclination: | 97.2851° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 155.5783° |
| argument of perigee: | 80.0075° |
| revolutions per day: | 15.33451362 |
| mean anomaly at epoch: | 280.1255° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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