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 04952U 26106.84170284 +.00000000 +00000-0 +42508-4 0 00005
2 04952 29.6681 296.0627 0079651 197.8041 182.6101 13.58635560 05
| Epoch (UTC): | 16 April 2026 20:12:03 |
| Eccentricity: | 0.0079651 |
| inclination: | 29.6681° |
| perigee height: | 982 km |
| apogee height: | 1100 km |
| right ascension of ascending node: | 296.0627° |
| argument of perigee: | 197.8041° |
| revolutions per day: | 13.58635560 |
| mean anomaly at epoch: | 182.6101° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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