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 49301U 26145.37300127 +.00000000 +00000-0 +11616-3 0 00009
2 49301 87.9175 278.9823 0002480 98.9695 261.1719 13.20771415 03
| Epoch (UTC): | 25 May 2026 08:57:07 |
| Eccentricity: | 0.0002480 |
| inclination: | 87.9175° |
| perigee height: | 1180 km |
| apogee height: | 1184 km |
| right ascension of ascending node: | 278.9823° |
| argument of perigee: | 98.9695° |
| revolutions per day: | 13.20771415 |
| mean anomaly at epoch: | 261.1719° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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