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 49139U 26145.18704475 +.00000000 +00000-0 +55356-4 0 00001
2 49139 70.0004 61.5682 0002710 263.7373 96.3477 14.98327698 01
| Epoch (UTC): | 25 May 2026 04:29:20 |
| Eccentricity: | 0.0002710 |
| inclination: | 70.0004° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 61.5682° |
| argument of perigee: | 263.7373° |
| revolutions per day: | 14.98327698 |
| mean anomaly at epoch: | 96.3477° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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