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 67659U 26145.36731170 +.00000000 +00000-0 +66553-3 0 00000
2 67659 97.2855 178.6179 0000147 193.1531 166.9708 15.33487983 03
| Epoch (UTC): | 25 May 2026 08:48:55 |
| Eccentricity: | 0.0000147 |
| inclination: | 97.2855° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 178.6179° |
| argument of perigee: | 193.1531° |
| revolutions per day: | 15.33487983 |
| mean anomaly at epoch: | 166.9708° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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