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 26053.81379248 +.00000000 +00000-0 +39869-4 0 00000
2 04952 29.6651 207.1745 0079377 124.9796 18.8531 13.58631409 04
| Epoch (UTC): | 22 February 2026 19:31:51 |
| Eccentricity: | 0.0079377 |
| inclination: | 29.6651° |
| perigee height: | 982 km |
| apogee height: | 1100 km |
| right ascension of ascending node: | 207.1745° |
| argument of perigee: | 124.9796° |
| revolutions per day: | 13.58631409 |
| mean anomaly at epoch: | 18.8531° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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