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 49503U 26132.05680531 +.00000000 +00000-0 +00000-0 0 00006
2 49503 62.8445 210.7069 6447392 272.5222 20.5946 2.00564720 06
| Epoch (UTC): | 12 May 2026 01:21:47 |
| Eccentricity: | 0.6447392 |
| inclination: | 62.8445° |
| perigee height: | 3058 km |
| apogee height: | 37307 km |
| right ascension of ascending node: | 210.7069° |
| argument of perigee: | 272.5222° |
| revolutions per day: | 2.00564720 |
| mean anomaly at epoch: | 20.5946° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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