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 48442U 26145.36674204 +.00000000 +00000-0 +96212-3 0 00008
2 48442 53.1599 180.9369 0001025 73.9841 286.1278 15.42227417 01
| Epoch (UTC): | 25 May 2026 08:48:06 |
| Eccentricity: | 0.0001025 |
| inclination: | 53.1599° |
| perigee height: | 439 km |
| apogee height: | 440 km |
| right ascension of ascending node: | 180.9369° |
| argument of perigee: | 73.9841° |
| revolutions per day: | 15.42227417 |
| mean anomaly at epoch: | 286.1278° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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