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 49103U 26145.34074576 +.00000000 +00000-0 +14308-2 0 00002
2 49103 87.8961 355.2112 0001070 80.6299 279.4951 13.12442204 09
| Epoch (UTC): | 25 May 2026 08:10:40 |
| Eccentricity: | 0.0001070 |
| inclination: | 87.8961° |
| perigee height: | 1213 km |
| apogee height: | 1215 km |
| right ascension of ascending node: | 355.2112° |
| argument of perigee: | 80.6299° |
| revolutions per day: | 13.12442204 |
| mean anomaly at epoch: | 279.4951° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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