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 49303U 26145.66269810 +.00000000 +00000-0 -10412-3 0 00000
2 49303 87.9176 278.9264 0002079 103.4546 256.6820 13.20770754 03
| Epoch (UTC): | 25 May 2026 15:54:17 |
| Eccentricity: | 0.0002079 |
| inclination: | 87.9176° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9264° |
| argument of perigee: | 103.4546° |
| revolutions per day: | 13.20770754 |
| mean anomaly at epoch: | 256.6820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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