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 68947U 26145.48838594 +.00000000 +00000-0 +10006-2 0 00003
2 68947 51.8742 176.8825 0003896 103.5878 256.5542 15.36227532 03
| Epoch (UTC): | 25 May 2026 11:43:16 |
| Eccentricity: | 0.0003896 |
| inclination: | 51.8742° |
| perigee height: | 455 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 176.8825° |
| argument of perigee: | 103.5878° |
| revolutions per day: | 15.36227532 |
| mean anomaly at epoch: | 256.5542° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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