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 49307U 26145.35617162 +.00000000 +00000-0 +45764-4 0 00005
2 49307 87.9176 278.9921 0002181 97.8624 262.2757 13.20772253 02
| Epoch (UTC): | 25 May 2026 08:32:53 |
| Eccentricity: | 0.0002181 |
| inclination: | 87.9176° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9921° |
| argument of perigee: | 97.8624° |
| revolutions per day: | 13.20772253 |
| mean anomaly at epoch: | 262.2757° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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