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 48298U 26145.52642149 +.00000000 +00000-0 +12362-2 0 00001
2 48298 53.1591 77.8850 0001663 109.9471 250.1710 15.33317218 09
| Epoch (UTC): | 25 May 2026 12:38:02 |
| Eccentricity: | 0.0001663 |
| inclination: | 53.1591° |
| perigee height: | 465 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 77.8850° |
| argument of perigee: | 109.9471° |
| revolutions per day: | 15.33317218 |
| mean anomaly at epoch: | 250.1710° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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