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 49304U 26145.37986683 +.00000000 +00000-0 +25852-3 0 00006
2 49304 87.9170 278.9887 0001992 96.6876 263.4484 13.20773325 00
| Epoch (UTC): | 25 May 2026 09:07:00 |
| Eccentricity: | 0.0001992 |
| inclination: | 87.9170° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9887° |
| argument of perigee: | 96.6876° |
| revolutions per day: | 13.20773325 |
| mean anomaly at epoch: | 263.4484° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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