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 40059U 26070.85051178 +.00000000 +00000-0 +14595-3 0 00008
2 40059 98.2095 13.6658 0001264 94.4969 265.6374 14.57097556 08
| Epoch (UTC): | 11 March 2026 20:24:44 |
| Eccentricity: | 0.0001264 |
| inclination: | 98.2095° |
| perigee height: | 702 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 13.6658° |
| argument of perigee: | 94.4969° |
| revolutions per day: | 14.57097556 |
| mean anomaly at epoch: | 265.6374° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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