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 67948U 26145.63918272 +.00000000 +00000-0 +54018-3 0 00004
2 67948 43.0018 115.7628 0001895 269.5575 90.5059 15.27599213 06
| Epoch (UTC): | 25 May 2026 15:20:25 |
| Eccentricity: | 0.0001895 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 115.7628° |
| argument of perigee: | 269.5575° |
| revolutions per day: | 15.27599213 |
| mean anomaly at epoch: | 90.5059° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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