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 49094U 26145.34921500 +.00000000 +00000-0 +91466-3 0 00000
2 49094 87.8960 355.2002 0001768 85.3840 274.7490 13.12440565 07
| Epoch (UTC): | 25 May 2026 08:22:52 |
| Eccentricity: | 0.0001768 |
| inclination: | 87.8960° |
| perigee height: | 1212 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.2002° |
| argument of perigee: | 85.3840° |
| revolutions per day: | 13.12440565 |
| mean anomaly at epoch: | 274.7490° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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