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 68670U 26145.14515541 +.00000000 +00000-0 +47944-3 0 00005
2 68670 97.2867 16.7007 0002184 86.0088 274.1404 15.33447740 04
| Epoch (UTC): | 25 May 2026 03:29:01 |
| Eccentricity: | 0.0002184 |
| inclination: | 97.2867° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 16.7007° |
| argument of perigee: | 86.0088° |
| revolutions per day: | 15.33447740 |
| mean anomaly at epoch: | 274.1404° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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