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 49002U 26145.50791432 +.00000000 +00000-0 -12438-3 0 00009
2 49002 87.9105 233.2753 0001903 110.0667 250.0669 13.16592698 04
| Epoch (UTC): | 25 May 2026 12:11:23 |
| Eccentricity: | 0.0001903 |
| inclination: | 87.9105° |
| perigee height: | 1196 km |
| apogee height: | 1199 km |
| right ascension of ascending node: | 233.2753° |
| argument of perigee: | 110.0667° |
| revolutions per day: | 13.16592698 |
| mean anomaly at epoch: | 250.0669° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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