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 62704U 26145.54901109 +.00000000 +00000-0 +11426-3 0 00006
2 62704 97.7028 223.9463 0006942 143.7477 216.4214 14.92753817 04
| Epoch (UTC): | 25 May 2026 13:10:34 |
| Eccentricity: | 0.0006942 |
| inclination: | 97.7028° |
| perigee height: | 585 km |
| apogee height: | 594 km |
| right ascension of ascending node: | 223.9463° |
| argument of perigee: | 143.7477° |
| revolutions per day: | 14.92753817 |
| mean anomaly at epoch: | 216.4214° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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