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 62800U 26145.61628734 +.00000000 +00000-0 +11842-3 0 00003
2 62800 88.9729 86.1053 0013576 216.1696 143.8539 13.51013716 08
| Epoch (UTC): | 25 May 2026 14:47:27 |
| Eccentricity: | 0.0013576 |
| inclination: | 88.9729° |
| perigee height: | 1058 km |
| apogee height: | 1079 km |
| right ascension of ascending node: | 86.1053° |
| argument of perigee: | 216.1696° |
| revolutions per day: | 13.51013716 |
| mean anomaly at epoch: | 143.8539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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