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 68894U 26144.86274007 +.00000000 +00000-0 +00000-0 0 00009
2 68894 2.6707 279.9915 1483211 180.9210 178.8850 1.35919146 08
| Epoch (UTC): | 24 May 2026 20:42:20 |
| Eccentricity: | 0.1483211 |
| inclination: | 2.6707° |
| perigee height: | 22941 km |
| apogee height: | 33154 km |
| right ascension of ascending node: | 279.9915° |
| argument of perigee: | 180.9210° |
| revolutions per day: | 1.35919146 |
| mean anomaly at epoch: | 178.8850° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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