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 00503U 26088.16528503 +.00000000 +00000-0 +00000-0 0 00005
2 00503 47.4933 167.6157 2839392 121.4471 289.5862 7.78168169 02
| Epoch (UTC): | 29 March 2026 03:58:00 |
| Eccentricity: | 0.2839392 |
| inclination: | 47.4933° |
| perigee height: | 1324 km |
| apogee height: | 7433 km |
| right ascension of ascending node: | 167.6157° |
| argument of perigee: | 121.4471° |
| revolutions per day: | 7.78168169 |
| mean anomaly at epoch: | 289.5862° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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