▸Orbital parameters

Orbit class	SSO
Inclination	97.6968°
Eccentricity	0.0001628
Period	94.8 min
Apogee	511 km
Perigee	509 km
Mean motion	15.18680231 rev/day
RAAN	275.2535°
Arg of perigee	221.1820°
Mean anomaly	138.9291°
B*	5.8657e-4
Rev at epoch	10,368

▸Two-line element set (TLE)

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

1 60541U 24149CB 26187.70672132 .00012102 00000-0 58657-3 0 9998

2 60541 97.6968 275.2535 0001628 221.1820 138.9291 15.18680231103681

▸ source OMM (JSON)

{
  "OBJECT_NAME": "UMBRA-09",
  "OBJECT_ID": "2024-149CB",
  "EPOCH": "2026-07-06T16:57:40.722+00:00",
  "MEAN_MOTION": 15.18680231,
  "ECCENTRICITY": 0.0001628,
  "INCLINATION": 97.6968,
  "RA_OF_ASC_NODE": 275.2535,
  "ARG_OF_PERICENTER": 221.182,
  "MEAN_ANOMALY": 138.9291,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 60541,
  "REV_AT_EPOCH": 10368,
  "BSTAR": 0.00058657,
  "MEAN_MOTION_DOT": 0.00012102,
  "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-09
Operator	Umbra LabsHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Aug 16, 2024HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	84HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/60541

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