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 26388U 26144.72683588 +.00000000 +00000-0 +00000-0 0 00004
2 26388 12.6477 31.5213 0005190 5.3612 191.9576 1.00271478 01
| Epoch (UTC): | 24 May 2026 17:26:38 |
| Eccentricity: | 0.0005190 |
| inclination: | 12.6477° |
| perigee height: | 35765 km |
| apogee height: | 35809 km |
| right ascension of ascending node: | 31.5213° |
| argument of perigee: | 5.3612° |
| revolutions per day: | 1.00271478 |
| mean anomaly at epoch: | 191.9576° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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