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 67670U 26145.35372234 +.00000000 +00000-0 -31754-4 0 00001
2 67670 97.2856 178.6383 0001512 93.4400 266.7015 15.33437978 07
| Epoch (UTC): | 25 May 2026 08:29:21 |
| Eccentricity: | 0.0001512 |
| inclination: | 97.2856° |
| perigee height: | 465 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 178.6383° |
| argument of perigee: | 93.4400° |
| revolutions per day: | 15.33437978 |
| mean anomaly at epoch: | 266.7015° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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