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 49176U 26145.47911661 +.00000000 +00000-0 -19136-4 0 00008
2 49176 70.0008 60.8399 0002742 261.7733 98.3115 14.98329267 01
| Epoch (UTC): | 25 May 2026 11:29:55 |
| Eccentricity: | 0.0002742 |
| inclination: | 70.0008° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 60.8399° |
| argument of perigee: | 261.7733° |
| revolutions per day: | 14.98329267 |
| mean anomaly at epoch: | 98.3115° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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