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 40057U 26111.53372580 +.00000000 +00000-0 +33804-3 0 00004
2 40057 98.2575 13.3359 0009225 97.7815 262.4453 14.97339951 00
| Epoch (UTC): | 21 April 2026 12:48:33 |
| Eccentricity: | 0.0009225 |
| inclination: | 98.2575° |
| perigee height: | 569 km |
| apogee height: | 582 km |
| right ascension of ascending node: | 13.3359° |
| argument of perigee: | 97.7815° |
| revolutions per day: | 14.97339951 |
| mean anomaly at epoch: | 262.4453° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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