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 67978U 26145.49696417 +.00000000 +00000-0 +83342-3 0 00007
2 67978 97.2849 155.5750 0001004 109.9741 250.1610 15.33452701 08
| Epoch (UTC): | 25 May 2026 11:55:37 |
| Eccentricity: | 0.0001004 |
| inclination: | 97.2849° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 155.5750° |
| argument of perigee: | 109.9741° |
| revolutions per day: | 15.33452701 |
| mean anomaly at epoch: | 250.1610° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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