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 00694U 26069.74934869 +.00000000 +00000-0 +22400-3 0 00006
2 00694 30.3513 189.7199 0547714 89.6263 276.7050 14.12071181 05
| Epoch (UTC): | 10 March 2026 17:59:03 |
| Eccentricity: | 0.0547714 |
| inclination: | 30.3513° |
| perigee height: | 456 km |
| apogee height: | 1248 km |
| right ascension of ascending node: | 189.7199° |
| argument of perigee: | 89.6263° |
| revolutions per day: | 14.12071181 |
| mean anomaly at epoch: | 276.7050° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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