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 48072U 26145.50695616 +.00000000 +00000-0 +11012-3 0 00008
2 48072 87.8945 324.7374 0001846 95.5271 264.6069 13.13468620 09
| Epoch (UTC): | 25 May 2026 12:10:01 |
| Eccentricity: | 0.0001846 |
| inclination: | 87.8945° |
| perigee height: | 1208 km |
| apogee height: | 1211 km |
| right ascension of ascending node: | 324.7374° |
| argument of perigee: | 95.5271° |
| revolutions per day: | 13.13468620 |
| mean anomaly at epoch: | 264.6069° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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