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 26150.86045815 +.00000000 +00000-0 +31473-3 0 00006
2 10703 99.3280 147.0202 0009706 22.5412 55.8931 13.99797045 03
| Epoch (UTC): | 30 May 2026 20:39:03 |
| Eccentricity: | 0.0009706 |
| inclination: | 99.3280° |
| perigee height: | 887 km |
| apogee height: | 902 km |
| right ascension of ascending node: | 147.0202° |
| argument of perigee: | 22.5412° |
| revolutions per day: | 13.99797045 |
| mean anomaly at epoch: | 55.8931° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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