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 49285U 26145.37468911 +.00000000 +00000-0 +18754-3 0 00006
2 49285 87.9175 278.9827 0002083 105.9993 254.1370 13.20771997 07
| Epoch (UTC): | 25 May 2026 08:59:33 |
| Eccentricity: | 0.0002083 |
| inclination: | 87.9175° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9827° |
| argument of perigee: | 105.9993° |
| revolutions per day: | 13.20771997 |
| mean anomaly at epoch: | 254.1370° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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