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 48304U 26145.29368969 +.00000000 +00000-0 +62923-4 0 00008
2 48304 53.1595 102.6149 0001170 87.3602 272.7533 15.31706032 04
| Epoch (UTC): | 25 May 2026 07:02:54 |
| Eccentricity: | 0.0001170 |
| inclination: | 53.1595° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 102.6149° |
| argument of perigee: | 87.3602° |
| revolutions per day: | 15.31706032 |
| mean anomaly at epoch: | 272.7533° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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