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 57936U 26145.39859199 +.00000000 +00000-0 -99464-5 0 00002
2 57936 53.1621 28.1212 0001397 98.3205 261.7954 15.30196270 01
| Epoch (UTC): | 25 May 2026 09:33:58 |
| Eccentricity: | 0.0001397 |
| inclination: | 53.1621° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 28.1212° |
| argument of perigee: | 98.3205° |
| revolutions per day: | 15.30196270 |
| mean anomaly at epoch: | 261.7954° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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