▸Orbital parameters

Orbit class	SSO
Inclination	97.6973°
Eccentricity	0.0001067
Period	94.8 min
Apogee	511 km
Perigee	509 km
Mean motion	15.18682750 rev/day
RAAN	275.5513°
Arg of perigee	172.5620°
Mean anomaly	187.5629°
B*	5.8089e-4
Rev at epoch	10,373

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 60547U 24149CH 26187.96983355 .00011984 00000-0 58089-3 0 9990

2 60547 97.6973 275.5513 0001067 172.5620 187.5629 15.18682750103735

▸ source OMM (JSON)

{
  "OBJECT_NAME": "UMBRA-10",
  "OBJECT_ID": "2024-149CH",
  "EPOCH": "2026-07-06T23:16:33.619+00:00",
  "MEAN_MOTION": 15.1868275,
  "ECCENTRICITY": 0.0001067,
  "INCLINATION": 97.6973,
  "RA_OF_ASC_NODE": 275.5513,
  "ARG_OF_PERICENTER": 172.562,
  "MEAN_ANOMALY": 187.5629,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60547,
  "REV_AT_EPOCH": 10373,
  "BSTAR": 0.00058089,
  "MEAN_MOTION_DOT": 0.00011984,
  "MEAN_MOTION_DDOT": 0
}

Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.

▸Satellite metadata

Name	UMBRA-10
Operator	Umbra LabsHIGHvia GCAT — Jonathan McDowell's General Catalog⚠ sources disagree UmbraMEDIUMvia Wikidata
Country	United StatesMEDIUMvia Wikidata
Launch date	Aug 16, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	84HIGH

▸Data quality

Score90 / 100

Claims9

Sources2

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org
WikidataCC0 1.0query.wikidata.org

▸Actions

GET /api/v1/satellites/60547

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.