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 40111U 26131.85970213 +.00000000 +00000-0 +27505-3 0 00000
2 40111 63.3763 113.3708 0387036 14.8696 346.3338 13.45447059 03
| Epoch (UTC): | 11 May 2026 20:37:58 |
| Eccentricity: | 0.0387036 |
| inclination: | 63.3763° |
| perigee height: | 800 km |
| apogee height: | 1378 km |
| right ascension of ascending node: | 113.3708° |
| argument of perigee: | 14.8696° |
| revolutions per day: | 13.45447059 |
| mean anomaly at epoch: | 346.3338° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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