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 53200U 26145.63791019 +.00000000 +00000-0 +44015-4 0 00005
2 53200 97.4455 206.6438 0002560 131.7355 228.4091 15.05653412 01
| Epoch (UTC): | 25 May 2026 15:18:35 |
| Eccentricity: | 0.0002560 |
| inclination: | 97.4455° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 206.6438° |
| argument of perigee: | 131.7355° |
| revolutions per day: | 15.05653412 |
| mean anomaly at epoch: | 228.4091° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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