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 63376U 26145.47394997 +.00000000 +00000-0 +58501-3 0 00000
2 63376 53.1572 65.8589 0001131 83.1960 276.9169 15.30204322 06
| Epoch (UTC): | 25 May 2026 11:22:29 |
| Eccentricity: | 0.0001131 |
| inclination: | 53.1572° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 65.8589° |
| argument of perigee: | 83.1960° |
| revolutions per day: | 15.30204322 |
| mean anomaly at epoch: | 276.9169° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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