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 49420U 26145.53936821 +.00000000 +00000-0 +13419-4 0 00009
2 49420 53.2138 244.1284 0000962 83.0736 277.0366 15.08837480 07
| Epoch (UTC): | 25 May 2026 12:56:41 |
| Eccentricity: | 0.0000962 |
| inclination: | 53.2138° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 244.1284° |
| argument of perigee: | 83.0736° |
| revolutions per day: | 15.08837480 |
| mean anomaly at epoch: | 277.0366° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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