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 65903U 26145.65932360 +.00000000 +00000-0 +11443-2 0 00003
2 65903 53.1601 14.1864 0001135 73.3357 286.7768 15.30222082 02
| Epoch (UTC): | 25 May 2026 15:49:25 |
| Eccentricity: | 0.0001135 |
| inclination: | 53.1601° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 14.1864° |
| argument of perigee: | 73.3357° |
| revolutions per day: | 15.30222082 |
| mean anomaly at epoch: | 286.7768° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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