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 48245U 26145.38011470 +.00000000 +00000-0 +12996-3 0 00008
2 48245 87.8948 294.2436 0001551 105.6001 254.5300 13.14501773 05
| Epoch (UTC): | 25 May 2026 09:07:21 |
| Eccentricity: | 0.0001551 |
| inclination: | 87.8948° |
| perigee height: | 1205 km |
| apogee height: | 1207 km |
| right ascension of ascending node: | 294.2436° |
| argument of perigee: | 105.6001° |
| revolutions per day: | 13.14501773 |
| mean anomaly at epoch: | 254.5300° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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