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 10703U 26038.98379689 +.00000000 +00000-0 +30855-3 0 00006
2 10703 99.3242 33.0230 0005625 338.0824 33.2887 13.99781086 02
| Epoch (UTC): | 07 February 2026 23:36:40 |
| Eccentricity: | 0.0005625 |
| inclination: | 99.3242° |
| perigee height: | 890 km |
| apogee height: | 899 km |
| right ascension of ascending node: | 33.0230° |
| argument of perigee: | 338.0824° |
| revolutions per day: | 13.99781086 |
| mean anomaly at epoch: | 33.2887° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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