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 25544U 26140.13305208 +.00000000 +00000-0 +96790-4 0 00003
2 25544 51.6329 78.9799 0007535 77.7466 282.4366 15.49278426 03
| Epoch (UTC): | 20 May 2026 03:11:35 |
| Eccentricity: | 0.0007535 |
| inclination: | 51.6329° |
| perigee height: | 414 km |
| apogee height: | 424 km |
| right ascension of ascending node: | 78.9799° |
| argument of perigee: | 77.7466° |
| revolutions per day: | 15.49278426 |
| mean anomaly at epoch: | 282.4366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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