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 60300U 26144.99679372 +.00000000 +00000-0 +41122-4 0 00005
2 60300 53.1606 57.9680 0001116 90.9960 269.1169 15.30184146 06
| Epoch (UTC): | 24 May 2026 23:55:22 |
| Eccentricity: | 0.0001116 |
| inclination: | 53.1606° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 57.9680° |
| argument of perigee: | 90.9960° |
| revolutions per day: | 15.30184146 |
| mean anomaly at epoch: | 269.1169° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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