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 26958U 26150.47996064 +.00000000 +00000-0 +21607-3 0 00001
2 26958 97.9602 158.3955 0054975 180.9813 179.1315 15.07421473 02
| Epoch (UTC): | 30 May 2026 11:31:08 |
| Eccentricity: | 0.0054975 |
| inclination: | 97.9602° |
| perigee height: | 506 km |
| apogee height: | 582 km |
| right ascension of ascending node: | 158.3955° |
| argument of perigee: | 180.9813° |
| revolutions per day: | 15.07421473 |
| mean anomaly at epoch: | 179.1315° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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