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 53048U 26145.47731816 +.00000000 +00000-0 +64164-3 0 00002
2 53048 97.4468 326.5447 0001415 114.2380 245.8995 15.05606092 07
| Epoch (UTC): | 25 May 2026 11:27:20 |
| Eccentricity: | 0.0001415 |
| inclination: | 97.4468° |
| perigee height: | 549 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 326.5447° |
| argument of perigee: | 114.2380° |
| revolutions per day: | 15.05606092 |
| mean anomaly at epoch: | 245.8995° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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