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 57386U 26145.47028947 +.00000000 +00000-0 +10273-3 0 00007
2 57386 99.5106 157.9096 0006562 176.1130 184.0143 15.06578477 07
| Epoch (UTC): | 25 May 2026 11:17:13 |
| Eccentricity: | 0.0006562 |
| inclination: | 99.5106° |
| perigee height: | 542 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 157.9096° |
| argument of perigee: | 176.1130° |
| revolutions per day: | 15.06578477 |
| mean anomaly at epoch: | 184.0143° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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