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 67739U 26145.57255307 +.00000000 +00000-0 +47382-3 0 00004
2 67739 97.2863 199.1710 0000811 297.2835 62.8325 15.33456115 03
| Epoch (UTC): | 25 May 2026 13:44:28 |
| Eccentricity: | 0.0000811 |
| inclination: | 97.2863° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 199.1710° |
| argument of perigee: | 297.2835° |
| revolutions per day: | 15.33456115 |
| mean anomaly at epoch: | 62.8325° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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