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 14248U 26150.25373146 +.00000000 +00000-0 +00000-0 0 00007
2 14248 11.1191 324.6103 0003913 55.3750 140.0218 0.98814776 01
| Epoch (UTC): | 30 May 2026 06:05:22 |
| Eccentricity: | 0.0003913 |
| inclination: | 11.1191° |
| perigee height: | 36183 km |
| apogee height: | 36217 km |
| right ascension of ascending node: | 324.6103° |
| argument of perigee: | 55.3750° |
| revolutions per day: | 0.98814776 |
| mean anomaly at epoch: | 140.0218° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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