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 57949U 26144.96054933 +.00000000 +00000-0 +48798-3 0 00002
2 57949 53.1615 29.7350 0001630 83.5672 276.5516 15.34323932 01
| Epoch (UTC): | 24 May 2026 23:03:11 |
| Eccentricity: | 0.0001630 |
| inclination: | 53.1615° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 29.7350° |
| argument of perigee: | 83.5672° |
| revolutions per day: | 15.34323932 |
| mean anomaly at epoch: | 276.5516° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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