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 49452U 26145.50813057 +.00000000 +00000-0 +37378-4 0 00006
2 49452 53.2136 234.3127 0001073 77.0421 283.0691 15.08838543 04
| Epoch (UTC): | 25 May 2026 12:11:42 |
| Eccentricity: | 0.0001073 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 234.3127° |
| argument of perigee: | 77.0421° |
| revolutions per day: | 15.08838543 |
| mean anomaly at epoch: | 283.0691° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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