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 26703U 26088.16054625 +.00000000 +00000-0 +17841-3 0 00008
2 26703 97.6900 106.8607 0007231 277.4637 82.5768 15.07404518 09
| Epoch (UTC): | 29 March 2026 03:51:11 |
| Eccentricity: | 0.0007231 |
| inclination: | 97.6900° |
| perigee height: | 539 km |
| apogee height: | 549 km |
| right ascension of ascending node: | 106.8607° |
| argument of perigee: | 277.4637° |
| revolutions per day: | 15.07404518 |
| mean anomaly at epoch: | 82.5768° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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