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 57402U 26145.58014000 +.00000000 +00000-0 +20955-3 0 00001
2 57402 97.2636 196.9998 0004109 192.8681 167.2456 15.29498758 02
| Epoch (UTC): | 25 May 2026 13:55:24 |
| Eccentricity: | 0.0004109 |
| inclination: | 97.2636° |
| perigee height: | 474 km |
| apogee height: | 480 km |
| right ascension of ascending node: | 196.9998° |
| argument of perigee: | 192.8681° |
| revolutions per day: | 15.29498758 |
| mean anomaly at epoch: | 167.2456° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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