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 49725U 26145.44739020 +.00000000 +00000-0 +94842-4 0 00008
2 49725 53.2117 164.6474 0000983 102.5913 257.5189 15.08847878 04
| Epoch (UTC): | 25 May 2026 10:44:14 |
| Eccentricity: | 0.0000983 |
| inclination: | 53.2117° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 164.6474° |
| argument of perigee: | 102.5913° |
| revolutions per day: | 15.08847878 |
| mean anomaly at epoch: | 257.5189° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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