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 49287U 26145.64906802 +.00000000 +00000-0 -41765-4 0 00004
2 49287 87.9177 278.9322 0001998 101.4862 258.6496 13.20773995 09
| Epoch (UTC): | 25 May 2026 15:34:39 |
| Eccentricity: | 0.0001998 |
| inclination: | 87.9177° |
| perigee height: | 1180 km |
| apogee height: | 1183 km |
| right ascension of ascending node: | 278.9322° |
| argument of perigee: | 101.4862° |
| revolutions per day: | 13.20773995 |
| mean anomaly at epoch: | 258.6496° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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